US20090324404A1 - Shear ring casing coupler device - Google Patents
Shear ring casing coupler device Download PDFInfo
- Publication number
- US20090324404A1 US20090324404A1 US12/215,184 US21518408A US2009324404A1 US 20090324404 A1 US20090324404 A1 US 20090324404A1 US 21518408 A US21518408 A US 21518408A US 2009324404 A1 US2009324404 A1 US 2009324404A1
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- Prior art keywords
- casing
- connector
- angled
- recess
- circumferential surface
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- 238000006073 displacement reaction Methods 0.000 claims abstract description 37
- 238000010276 construction Methods 0.000 description 27
- 239000012530 fluid Substances 0.000 description 4
- 238000009434 installation Methods 0.000 description 2
- 230000000295 complement effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000008676 import Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/62—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps
- F04D29/624—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/39—Retaining components in desired mutual position by a V-shaped ring to join the flanges of two cylindrical sections, e.g. casing sections of a turbocharger
Definitions
- the present invention relates to fluid machinery, and more particularly to high pressure casings for such machinery.
- Fluid machinery such as centrifugal compressors each typically includes a casing for containing working components such as one or more impellers mounted on a rotatable shaft.
- the casing includes one or more inlets for directing fluid inwardly toward the compressor working components and one or more outlets for directing pressurized fluid outwardly from the casing for subsequent processing or ultimate usage.
- casings are often formed as an assembly of two or more separate casings, such as a first casing for housing the compression working components and a second casing for housing a driver (e.g., electric motor, gas turbine, etc.).
- the casing assembly requires one or more coupler devices to connect adjacent pairs of the casings, which generally must enable removable coupling of the casings to permit periodic maintenance and/or repair of the compressor or driver components.
- the present invention is a coupler device for connecting first and second casings to form a casing assembly with a central axis, each casing having an inner end disposed against the inner end of the other casing such that the casings are spaced along the axis.
- the coupler device comprises at least one generally arcuate connector having a first portion engageable with the first casing and a second portion engageable with the second casing so as to connect the two casings.
- the connector extends at least partially circumferentially about the casing axis.
- a retainer is disposeable either generally within or generally about the connector and is configured to prevent radial displacement of the connector with respect to the axis so as to maintain engagement of the connector with the first and second casings.
- the present invention is a casing assembly comprising first and second casings, each one of the first and second casings having an inner end disposed one of generally against the inner end of the other one of the two casings and generally proximal to the inner end of the other one of the two casings.
- the two casings are generally centered about and spaced along a central longitudinal axis.
- a coupler device includes at least one generally arcuate connector having a first portion engageable with the first casing and a second portion engageable with the second casing so as to connect the two casings.
- the connector extends at least partially circumferentially about the casing axis.
- a retainer is disposeable either generally within or generally about the connector and is configured to prevent radial displacement of the connector with respect to the axis so as to maintain engagement of the connector with the first and second casings.
- the present invention is again a coupler device for connecting first and second casings to form a casing assembly with a central axis, each casing having an inner end disposed against the inner end of the other casing such that the casings are spaced along the axis and a recess located adjacent to the casing end.
- the coupler device comprises at least one generally arcuate connector having a first lug engageable with the first casing recess and a second lug engageable with the second casing recess so as to connect the two casings.
- the connector further includes first and second angled surface sections each facing generally away from the other angled surface section. The connector extends at least partially circumferentially about the casing axis.
- a retainer is disposeable generally within or generally about the at least one connector and is configured to prevent radial displacement of the connector with respect to the axis so as to maintain the first and second lugs engaged with the casing recesses.
- the retainer includes first and second axially spaced members, each connector member having an angled outer circumferential surface facing generally toward the angled surface of the other one of the first and second connector members. Furthermore, the retainer first member angled surface is disposeable against the connector first angled surface section and the retainer second member angled surface is disposeable against the connector second angled inner surface section.
- the first and second retainer members are adjustably connected such that the two retainer members are displaceable generally toward each other so as to bias the connector generally radially with respect to the casing axis to engage the retainer lugs with the casing recesses.
- FIG. 1 is a broken-away, perspective view of a coupler device and casing assembly in accordance with a first construction of the present invention
- FIG. 2 is an enlarged view of a portion of FIG. 1 ;
- FIG. 3 is a broken-away, axial cross-sectional view of the first construction coupler device and casing assembly
- FIG. 4 is a broken-away, perspective view of the coupler device and casing assembly in accordance with a second construction of the present invention
- FIG. 5 is a broken-away, axial cross-sectional view of the second construction coupler device and casing assembly
- FIG. 6 is a broken-away, perspective view of the coupler device and casing assembly in accordance with a third construction of the present invention.
- FIG. 7 is a broken-away, axial cross-sectional view of the third construction coupler device and casing assembly
- FIG. 8 is a broken-away, perspective view of the coupler device and casing assembly in accordance with a fourth construction of the present invention.
- FIG. 9 is a broken-away, axial cross-sectional view of the first construction coupler device and casing assembly.
- FIGS. 1-9 a coupler device 10 for connecting first and second casings 12 , 14 to form a casing assembly 20 with a central longitudinal axis 21 .
- Each casing 12 , 14 has an inner end 12 a, 14 a disposed against, or located at least generally proximal to, the inner end 14 a, 12 a of the other casing 14 , 12 , respectively, such that the casings 12 , 14 are generally centered about and spaced along the axis 21 .
- the coupler device 10 basically includes at least one and preferably a plurality of generally arcuate connectors 22 and a retainer 24 .
- Each connector 22 has a first portion 22 a engageable with the first casing 12 and a second portion 22 b engageable with the second casing 14 so as to connect the two casings 12 , 14 , such the casing inner ends 12 a, 14 a generally fixed together or immovably attached.
- each connector 22 extends at least partially circumferentially about the casing axis 21 , the plurality of connectors being circumferentially spaced about the axis.
- the retainer 24 is disposeable either generally within ( FIGS. 1 and 2 ) or generally about ( FIGS. 3-8 ) the connector 22 and is configured to prevent radial displacement of the connector 22 with respect to the axis 21 so as to maintain engagement of the connector 22 with the first and second casings 12 , 14 .
- each one of the first and second casings 12 , 14 has a recess 16 , 18 , respectively and the connector first portion 22 a includes a first lug 30 disposeable within the first casing recess 16 and the connector second portion 22 b includes a second lug 32 disposeable within the second casing recess 18 .
- the retainer 14 is basically configured to maintain the first and second lugs 30 , 32 disposed within the first and second casing recesses 16 , 18 , respectively. More specifically, each casing 12 , 14 has at least an inner circumferential surface 13 A, 15 A, respectively and/or at least an outer circumferential surface 13 B, 15 B, respectively, and preferably both the inner and outer circumferential surfaces.
- each casing recess 16 , 18 extends either radially outwardly from the casing inner circumferential surface 13 A, 15 A ( FIGS. 1-3 ) or radially inwardly from the casing outer circumferential surface 13 B, 15 B ( FIGS. 4-9 ). In either arrangement, each casing recess 16 , 18 also preferably extends circumferentially entirely about the casing axis 21 .
- each connector portion lug 30 , 32 extends either generally radially outwardly from a remainder of the connector 22 so as to be disposeable within a separate one of the radially-outwardly extending casing recesses 16 , 18 or radially inwardly from a remainder of the connector 30 so as to be disposeable within a separate one of the radially-inwardly extending casing recesses 16 , 18 .
- the retainer 24 is configured to either prevent displacement of the connector 22 in a radial direction generally toward the casing axis 21 to maintain the connector lugs 30 , 32 engaged with radially-outwardly extending casing recesses 16 , 18 or to prevent displacement of the connector 22 in a radial direction generally away from the casing axis 21 to maintain the connector lugs 30 , 32 engaged with radially-inwardly extending casing recesses 16 , 18 .
- the connector 22 has a pair of angled, generally opposing contact surfaces or surface sections 34 A, 34 B
- the retainer 24 includes first and second axially spaced, generally annular members 36 A, 36 B each having an angled “drive” surface 37 A, 37 B disposed generally against a separate one of the connector angled contact surfaces 34 A, 34 B, respectively.
- the retainer first and second members 36 A, 36 B are adjustably connected such that the two retainers members 36 A, 36 B are displaceable generally toward each other along the axis 21 so as to bias the connector 24 either generally radially outwardly toward the casing inner surfaces 13 A, 15 A, or radially inwardly toward the casing outer surfaces 13 B, 15 B, as described in further detail below.
- the retainer 24 includes two “overlapping” annular members 40 , 42 or may include a plurality of threaded rods or fasteners 44 , as shown in FIGS. 8 and 9 .
- the coupler device 10 engages with the casing inner surfaces 13 A, 15 A, and is thus disposed within an interior chamber C C of the casing assembly 20 .
- each casing recess 16 , 18 extends radially outwardly from the inner circumferential surface 13 A, 15 A, respectively, of the particular casing 12 , 14 and each connector portion lug 30 , 32 extends radially outwardly from a remainder of the connector 22 , with the retainer 24 being configured to prevent displacement of the connector 22 in a radial direction R 1 generally toward the casing axis 21 .
- each casing recess 16 , 18 is partially defined by an angled radial contact surface 46 A, 46 B, a facing radial surface 47 A, 47 B, and an inner circumferential surface 48 A, 48 B extending axially between the radial surfaces, the three surfaces 46 , 47 and 48 extending circumferentially about the casing axis 21 .
- Each one of the two casing recess angled contact surfaces 46 A, 46 B face generally away from the other one of the two casing recess angled surfaces 46 B, 46 A, for reasons discussed below.
- each connector 22 includes a generally arcuate body 50 with two opposing axial ends 50 a, 50 b, opposing radial ends 50 c (only one shown) and inner and outer circumferential surfaces 51 A, 51 B.
- the first and second lugs 30 , 32 extend from the outer surface 5 B and each preferably includes a generally rectangular shoulder 52 extending circumferentially between the radial ends 50 c, the two shoulders 52 being spaced apart and each located generally adjacent to a separate one of the axial ends 50 a or 50 b.
- each one of the first and second connector lugs 30 , 32 has an angled drive surface 53 A, 53 B formed on the annular shoulder 52 and extending at least partially circumferentially about the casing axis 21 .
- Each one of the two lug angled drive surfaces 53 A, 53 B faces generally toward the other one of the two lug angled surfaces 53 B, 53 A, respectively. Furthermore, the first lug angled surface 53 A is disposed against the first casing recess angled contact surface 46 A and the second lug angled surface 53 B is disposed against the second casing recess angled surface 46 B.
- the connector angled contact surface sections 34 A, 34 B are formed or provided on the body inner surface 51 A and extend circumferentially between the body radial ends 50 c.
- Each contact surface 34 A or 34 B faces generally toward an adjacent one of the two axial ends 50 a, 50 b, respectively, and generally away from the other angled surface section 34 B, 34 A, respectively, for reasons described in detail below.
- the retainer 24 of the first coupler construction has first and second retainer members 36 A, 36 B that each include a generally annular body 54 , 56 , respectively.
- Each retainer annular body 54 , 56 has an inner axial end 56 a, 56 a, an outer axial end 54 b, 56 b, an inner circumferential surface 55 A, 57 A, and an outer circumferential surface 55 B, 57 B providing one of the angled drive surfaces 37 A, 37 B.
- the two annular bodies 54 , 56 are arranged such that the body inner ends 56 are disposed at least generally adjacent to each other and each angled drive surface 37 A, 37 B faces generally toward the angled surface 37 B, 37 A on the other retainer body 56 , 54 .
- the two retainer bodies 54 , 56 are sized to be disposed radially inwardly of the connector body 50 such that the retainer first angled outer surface 37 A is disposed against the connector first angled inner surface section 34 A and the retainer second angled outer surface 37 B is disposed against the connector second angled inner surface section 34 B. As such, axial movement of the retainer bodies 54 , 56 displaces the connector 12 radially, as described below.
- the two retainer bodies 54 , 56 are preferably adjustably connected by a plurality of threaded rods 58 extending axially through the second body 56 and secured within the first body 54 and a plurality of nuts 59 each engageable with the rod 58 and contactable with the outer end 56 b of the second body 56 .
- the rods 58 and nuts 59 are spaced circumferentially apart on the two bodies 54 , 56 , as best shown in FIG. 2 .
- each nut 59 in a first angular direction A 1 displaces each retainer body 54 , 56 generally toward the other body 56 , 54
- rotation of the nuts 59 in a second angular direction A 2 enables each body 54 , 56 to displace generally away from the other body 56 , 54 .
- each retainer body 54 , 56 displacement of the retainer bodies 54 , 56 axially away from each other cause each retainer angled drive surface 37 A, 37 B to displace away from each other, which enables the connectors 22 to displace radially inwardly.
- Such radial inward displacement of the connectors 22 cause the connector lugs 30 , 32 to withdraw from the casing recesses 16 , 18 , thereby disconnecting the casing ends 12 a, 14 a.
- the first construction of the coupler device 10 also preferably comprises a generally tubular guide member 49 disposed radially inwardly of the retainer 24 and configured to generally retain the connectors 22 disposed adjacent to the casing recesses 16 , 18 during installation and removal of the coupler device 10 .
- the guide member 49 at least temporarily supports the plurality of connectors 22 prior to insertion of the two retainer bodies 54 , 56 between the guide member 49 and the connectors 22 and after removal of the retainer bodies 54 , 56 during casing disassembly, Referring now to FIGS.
- each casing recess 16 , 18 extends radially inwardly from the outer circumferential surface 13 B, 15 B, respectively, of the particular casing 12 , 14 and each connector portion lug 30 , 32 extends radially inwardly from a remainder of the connector 22 , with the retainer 24 being configured to prevent displacement of the connector 22 in a radial direction R 2 generally away from the casing axis 21 .
- each casing recess 16 , 18 is partially defined by an angled radial contact surface 60 A, 60 B, a facing radial surface 61 A, 61 B, and an outer circumferential surface section 62 A, 62 B extending axially between the radial surfaces, the three surfaces 60 , 61 and 62 extending circumferentially about the casing axis 21 .
- Each one of the two casing recess angled contact surfaces 60 A, 60 B faces generally away from the other one of the two casing recess angled surfaces 60 B, 60 A, for reasons discussed below.
- each connector 22 includes a generally arcuate body 64 with two opposing axial ends 64 a, 64 b, opposing radial ends 64 c, and inner and outer circumferential surfaces 65 A, 65 B.
- the first and second lugs 30 , 32 extend from the body inner surface 65 A and each preferably includes a generally rectangular shoulder 66 extending circumferentially between the radial ends 64 c, the two shoulders 64 being spaced apart and each located generally adjacent to a separate one of the axial ends 64 a or 64 b.
- each one of the first and second connector lugs 30 , 32 has an angled drive surface 68 A, 68 B formed on the annular shoulder 66 and extending at least partially circumferentially about and facing generally towards the casing axis 21 .
- Each one of the two lug angled drive surfaces 68 A, 68 B also faces generally toward the other one of the two lug angled surfaces 68 B, 68 A, respectively.
- the first lug angled surface 68 A is disposeable or disposed against the first casing recess angled contact surface 60 A and the second lug angled surface 68 B is disposeable/disposed against the second casing recess angled surface 60 B.
- each connector angled contact surface section 34 A, 34 B are formed or provided on the outer surface 65 B of each connector body 64 , extend circumferentially between the body radial ends 64 c and face generally away from the casing axis 21 .
- Each connector contact surface 34 A or 34 B also faces generally toward an adjacent one of the two axial ends 64 a, 64 b, respectively, and generally away from the other angled surface section 34 B, 34 A, respectively, for reasons described in detail below.
- the retainer 24 of the second coupler construction has first and second retainer members 36 A, 36 B that each include a generally annular body 70 , 72 , respectively.
- Each retainer annular body 70 , 72 has an inner axial end 70 a, 72 a, an outer axial end 70 b, 72 b, an inner circumferential surface 71 A, 73 A providing one of the angled drive surfaces 37 A, 37 B, and an outer circumferential surface 71 B, 73 B.
- the two annular bodies 70 , 72 are arranged such that the body inner ends 70 a, 72 a are disposed at least generally adjacent to each other and each angled drive surface 37 A, 37 B faces generally toward the angled surface 37 B, 37 A on the other retainer body 72 , 70 .
- the two retainer bodies 70 , 72 are sized to be disposed radially outwardly of the connector body 64 , and are thus diametrically larger than the casing outer surfaces 13 B, 15 B, and are arrangeable/arranged such that the retainer first angled inner surface 37 A is disposed against the connector first angled outer surface section 34 A and the retainer second angled inner surface 37 B is disposed against the connector second angled outer surface section 34 B.
- axial movement of the retainer bodies 70 , 72 displaces the connector 12 radially, as described below.
- the first retainer body 70 is generally tubular and has three sections: an outer, angled section 71 a providing the angled drive surface 37 A, an inner, radially enlarged section 71 b having a plurality of “blind holes” 76 (one shown), as discussed below, and a central portion 71 c extending axially between and connecting the inner and outer sections 71 a, 71 b.
- the second retainer body 72 is preferably formed as a generally rectangular ring with the angled drive surface 37 b extending axially entirely along the body inner surface 73 .
- each of the retainer bodies 70 , 72 is preferably formed of a plurality of semicircular, partial-circular or arcuate sections (not indicated), so as to facilitate installation about the connectors 22 , but may alternatively be provided by one-piece annular bodies or rings.
- the two retainer bodies 70 , 72 are preferably adjustably connected by a plurality of threaded rods 74 extending axially through the second body 72 and secured within a separate one of the blind holes 76 of the first body 70 and a plurality of nuts 75 each engaged with the rod 74 and contactable with the outer end 72 b of the second body 72 .
- the rods 74 and threaded openings are spaced circumferentially apart on the two bodies 70 , 72 , as best shown in FIG. 4 .
- each nut 75 in a first angular direction A 1 displaces each retainer body 70 , 72 generally toward the other body 72 , 70
- rotation of the nuts 75 in a second angular direction A 2 enables each body 70 , 72 to be displaced generally away from the other body 72 , 70 .
- each retainer body 70 , 72 displacement of the retainer bodies 70 , 72 axially away from each other cause each retainer angled drive surface 37 A, 37 B to displace away from each other, which enables the connectors 22 to displace radially outwardly.
- Such radial outward displacement of the connectors 22 permits the connector lugs 30 , 32 to be withdrawn from the casing recesses 16 , 18 , thereby disconnecting the casing ends 12 a, 14 a.
- each casing recess 16 , 18 extends radially inwardly from the outer circumferential surface 13 B, 15 B, respectively, of the particular casing 12 , 14 and each connector portion lug 30 , 32 extends radially inwardly from a remainder of the connector 22 , with the retainer 24 being configured to prevent displacement of the connector 22 in a radial direction R 2 generally away from the casing axis 21 .
- each casing recess 16 , 18 is partially defined by an angled radial contact surface 80 A, 80 B, a facing radial surface 81 A, 81 B, and an outer circumferential surface section 82 A, 82 B extending axially between the radial surfaces, the three surfaces 80 , 81 and 82 extending circumferentially about the casing axis 21 .
- Each one of the two casing recess angled contact surfaces 80 A, 80 B faces generally away from the other one of the two casing recess angled surfaces 80 B, 80 A, for reasons as discussed above with the second construction and in further detail below.
- each connector 22 includes a generally arcuate body 84 with two opposing axial ends 84 a, 84 b, opposing radial ends 84 c (only one shown) and inner and outer circumferential surfaces 85 A, 85 B.
- the first and second lugs 30 , 32 extend from the body inner surface 85 A and each preferably includes a generally rectangular, annular body portion 86 extending circumferentially between the radial ends 84 c, the two annular body portions 86 being axially spaced apart and each located generally adjacent to a separate one of the axial ends 84 a or 84 b.
- each one of the first and second connector lugs 30 , 32 has an angled drive surface 88 A, 88 B formed on the annular body portion 86 and extending at least partially circumferentially about and facing generally towards the casing axis 21 .
- Each one of the two lug angled drive surfaces 88 A, 88 B also faces generally toward the other one of the two lug angled surfaces 88 B, 88 A, respectively.
- the first lug angled surface 88 A is disposeable or disposed against the first casing recess angled contact surface 80 A and the second lug angled surface 88 B is disposeable/disposed against the second casing recess angled surface 80 B.
- each connector body 84 is formed without angled contact surfaces engageable by the retainer 24 . Rather, the body outer circumferential surface 85 B is substantially “radially constant”, i.e., the body outside radius does not vary on the outer surface 85 B.
- the retainer 24 of the third coupler construction has first and second retainer members 36 A, 36 B that include inner and outer generally annular members 90 , 92 , respectively.
- Each generally annular member 90 , 92 has an opposing axial ends 90 a, 92 a, an inner circumferential surface 91 A, 93 A and an outer circumferential surface 91 B, 93 B, respectively.
- the inner member 90 is disposed generally between the connector body 84 and the outer member 92 such that the inner member inner surface 91 A is disposed against the connector body outer surface 85 B and the inner member outer surface 91 B is disposed against the outer member inner surface 93 A.
- the inner member outer surface 91 B and the outer member inner surface 93 A are each generally angled and arranged such that each surface 91 B, 93 A faces generally toward the other surface 93 A, 91 B and are juxtaposeable against each other.
- axial displacement of the outer member 92 relative to the inner member 90 in a first axial direction D 1 biases the inner member 90 generally radially inwardly toward the connector 22 . That is, as the outer body 92 displaces axially in the first direction D 1 , the outer body inner surface 93 A, slides against the inner body outer surface 91 B and forces the inner body 90 to displace or at least compress radially inwardly. Thereby, the inner member 90 exerts a radially inwardly directed force F on the connector 22 such that the connector lug drive surfaces 88 A, 88 B slide along or are at least biased against, the casing recess contact surfaces 80 A, 80 B as discussed above.
- axial displacement of the outer member 92 relative to the inner member 90 in a second, opposing axial direction D 2 removes the radially-inwardly directed compressive force on the inner body 90 , thereby permitting removal of the inner body 90 and thereafter the connector 22 so as to disengage the lugs 30 , 32 from the casing recesses 16 , 18 .
- the coupler device 10 is disposed externally of the casings 12 , 14 and engages with the casing outer surfaces 13 B, 15 B, as with the second and third constructions.
- each casing recess 16 , 18 extends radially inwardly from the outer circumferential surface 13 B, 15 B, respectively, of the particular casing 12 , 14
- each connector portion lug 30 , 32 extends radially inwardly from a remainder of the connector 22
- the retainer 24 is configured to prevent displacement of the connector 22 in a radial direction R 2 generally away from the casing axis 21 .
- each casing recess 16 , 18 is partially defined by an angled radial contact surface 100 A, 100 B, a facing radial surface 101 A, 101 B, and an outer circumferential surface section 102 A, 102 B extending axially between the radial surfaces, the three surfaces 100 , 101 and 102 extending circumferentially about the casing axis 21 .
- Each one of the two casing recess angled contact surfaces 100 A, 100 B faces generally away from the other one of the two casing recess angled surfaces 100 B, 100 A, so as to engage with complementary lug drive surfaces 108 , 108 B in a manner discussed below.
- each connector 22 includes a generally rectangular bar 104 having opposing axial ends 104 a, 104 b, opposing radial ends 104 c and inner and outer surfaces 105 A, 105 B.
- Each rectangular bar 104 is sized substantially “circumferentially smaller”, i.e., has a much lesser circumferential extent, in comparison with the connector bodies 50 , 64 , 84 of the first, second, and third constructions, respectively. As such, the fourth construction has a greater number of the connectors 22 in comparison with the previously described constructions.
- first and second connector lugs 30 , 32 extend from the body inner surface 105 A and each preferably includes a generally rectangular body portion 106 extending circumferentially between the radial ends 104 c, the two annular body portions 106 being axially spaced apart and each located generally adjacent to a separate one of the axial ends 104 a or 104 b.
- each one of the first and second connector lugs 30 , 32 has an angled drive surface 108 A, 108 B formed on the rectangular body portion 106 and extending at least partially circumferentially about and facing generally towards the casing axis 21 .
- Each one of the two lug angled drive surfaces 108 A, 108 B also faces generally toward the other one of the two lug angled surfaces 108 B, 108 A, respectively. Furthermore, the first lug angled surface 108 A is disposeable or disposed against the first casing recess angled contact surface 100 A and the second lug angled surface 108 B is disposeable/disposed against the second casing recess angled surface 100 B.
- displacement of the connector 22 in the radially inward direction R 2 biases the end 12 a or 14 a of each one of the first and second casings 12 , 14 generally toward the end 12 a, 14 a of the other one of the first and second casings 12 , 14 , in a manner generally similar with the second and third coupler and casing constructions.
- the fourth construction of the coupler device 10 preferably includes a plurality of retainers 24 , most preferably two retainers 24 for each connector 22 .
- each retainer 24 preferably includes a threaded rod or fastener 110 and a nut 112 engageable with the rod 110 .
- Each rod 110 has a first end 110 a connected with the one of the casings 12 , 14 and a second end 110 b extending outwardly of the connector body 84 , the second end 110 b being threaded so as to be engageable by the nut.
- each nut 112 clamps against the connector body outer surface 105 B, so as to force the connector lugs 30 , 32 to displace radially inwardly to connect the casing ends 12 a, 14 a.
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Abstract
Description
- The present invention relates to fluid machinery, and more particularly to high pressure casings for such machinery.
- Fluid machinery such as centrifugal compressors each typically includes a casing for containing working components such as one or more impellers mounted on a rotatable shaft. The casing includes one or more inlets for directing fluid inwardly toward the compressor working components and one or more outlets for directing pressurized fluid outwardly from the casing for subsequent processing or ultimate usage. Further, such casings are often formed as an assembly of two or more separate casings, such as a first casing for housing the compression working components and a second casing for housing a driver (e.g., electric motor, gas turbine, etc.). As such, the casing assembly requires one or more coupler devices to connect adjacent pairs of the casings, which generally must enable removable coupling of the casings to permit periodic maintenance and/or repair of the compressor or driver components.
- In one aspect, the present invention is a coupler device for connecting first and second casings to form a casing assembly with a central axis, each casing having an inner end disposed against the inner end of the other casing such that the casings are spaced along the axis. The coupler device comprises at least one generally arcuate connector having a first portion engageable with the first casing and a second portion engageable with the second casing so as to connect the two casings. The connector extends at least partially circumferentially about the casing axis. Further, a retainer is disposeable either generally within or generally about the connector and is configured to prevent radial displacement of the connector with respect to the axis so as to maintain engagement of the connector with the first and second casings.
- In another aspect, the present invention is a casing assembly comprising first and second casings, each one of the first and second casings having an inner end disposed one of generally against the inner end of the other one of the two casings and generally proximal to the inner end of the other one of the two casings. The two casings are generally centered about and spaced along a central longitudinal axis. A coupler device includes at least one generally arcuate connector having a first portion engageable with the first casing and a second portion engageable with the second casing so as to connect the two casings. The connector extends at least partially circumferentially about the casing axis. Further, a retainer is disposeable either generally within or generally about the connector and is configured to prevent radial displacement of the connector with respect to the axis so as to maintain engagement of the connector with the first and second casings.
- In a further aspect, the present invention is again a coupler device for connecting first and second casings to form a casing assembly with a central axis, each casing having an inner end disposed against the inner end of the other casing such that the casings are spaced along the axis and a recess located adjacent to the casing end. The coupler device comprises at least one generally arcuate connector having a first lug engageable with the first casing recess and a second lug engageable with the second casing recess so as to connect the two casings. The connector further includes first and second angled surface sections each facing generally away from the other angled surface section. The connector extends at least partially circumferentially about the casing axis. Further, a retainer is disposeable generally within or generally about the at least one connector and is configured to prevent radial displacement of the connector with respect to the axis so as to maintain the first and second lugs engaged with the casing recesses. The retainer includes first and second axially spaced members, each connector member having an angled outer circumferential surface facing generally toward the angled surface of the other one of the first and second connector members. Furthermore, the retainer first member angled surface is disposeable against the connector first angled surface section and the retainer second member angled surface is disposeable against the connector second angled inner surface section. The first and second retainer members are adjustably connected such that the two retainer members are displaceable generally toward each other so as to bias the connector generally radially with respect to the casing axis to engage the retainer lugs with the casing recesses.
- The foregoing summary, as well as the detailed description of the preferred embodiments of the present invention, will be better understood when read in conjunction with the appended drawings. For the purpose of illustrating the invention, there is shown in the drawings, which are diagrammatic, embodiments that are presently preferred. It should be understood, however, that the present invention is not limited to the precise arrangements and instrumentalities shown. In the drawings:
-
FIG. 1 is a broken-away, perspective view of a coupler device and casing assembly in accordance with a first construction of the present invention; -
FIG. 2 is an enlarged view of a portion ofFIG. 1 ; -
FIG. 3 is a broken-away, axial cross-sectional view of the first construction coupler device and casing assembly; -
FIG. 4 is a broken-away, perspective view of the coupler device and casing assembly in accordance with a second construction of the present invention; -
FIG. 5 is a broken-away, axial cross-sectional view of the second construction coupler device and casing assembly -
FIG. 6 is a broken-away, perspective view of the coupler device and casing assembly in accordance with a third construction of the present invention; -
FIG. 7 is a broken-away, axial cross-sectional view of the third construction coupler device and casing assembly; -
FIG. 8 is a broken-away, perspective view of the coupler device and casing assembly in accordance with a fourth construction of the present invention; and -
FIG. 9 is a broken-away, axial cross-sectional view of the first construction coupler device and casing assembly. - Certain terminology is used in the following description for convenience only and is not limiting. The words “right”, left”, “lower”, “upper”, “upward”, “down” and “downward” designate directions in the drawings to which reference is made. The words “inner”, “inwardly” and “outer”, “outwardly” refer to directions toward and away from, respectively, a designated centerline or a geometric center of an element being described, the particular meaning being readily apparent from the context of the description. Further, as used herein, the word “connected” is intended to include direct connections between two members without any other members interposed therebetween and indirect connections between members in which one or more other members are interposed therebetween. The terminology includes the words specifically mentioned above, derivatives thereof, and words of similar import.
- Referring now to the drawings in detail, wherein like numbers are used to indicate like elements throughout, there is shown in
FIGS. 1-9 acoupler device 10 for connecting first and 12, 14 to form asecond casings casing assembly 20 with a centrallongitudinal axis 21. Each 12, 14 has ancasing 12 a, 14 a disposed against, or located at least generally proximal to, theinner end 14 a, 12 a of theinner end 14, 12, respectively, such that theother casing 12, 14 are generally centered about and spaced along thecasings axis 21. Thecoupler device 10 basically includes at least one and preferably a plurality of generallyarcuate connectors 22 and aretainer 24. Eachconnector 22 has a first portion 22 a engageable with thefirst casing 12 and asecond portion 22 b engageable with thesecond casing 14 so as to connect the two 12, 14, such the casingcasings 12 a, 14 a generally fixed together or immovably attached. Also, eachinner ends connector 22 extends at least partially circumferentially about thecasing axis 21, the plurality of connectors being circumferentially spaced about the axis. Further, theretainer 24 is disposeable either generally within (FIGS. 1 and 2 ) or generally about (FIGS. 3-8 ) theconnector 22 and is configured to prevent radial displacement of theconnector 22 with respect to theaxis 21 so as to maintain engagement of theconnector 22 with the first and 12, 14.second casings - Preferably, each one of the first and
12, 14 has asecond casings 16, 18, respectively and the connector first portion 22 a includes arecess first lug 30 disposeable within thefirst casing recess 16 and the connectorsecond portion 22 b includes asecond lug 32 disposeable within thesecond casing recess 18. With this preferred structure, theretainer 14 is basically configured to maintain the first and 30, 32 disposed within the first andsecond lugs 16, 18, respectively. More specifically, eachsecond casing recesses 12, 14 has at least an innercasing 13A, 15A, respectively and/or at least an outercircumferential surface 13B, 15B, respectively, and preferably both the inner and outer circumferential surfaces. Further, each casing recess 16, 18 extends either radially outwardly from the casing innercircumferential surface 13A, 15A (circumferential surface FIGS. 1-3 ) or radially inwardly from the casing outer 13B, 15B (circumferential surface FIGS. 4-9 ). In either arrangement, each casing recess 16, 18 also preferably extends circumferentially entirely about thecasing axis 21. - Furthermore, each
30, 32 extends either generally radially outwardly from a remainder of theconnector portion lug connector 22 so as to be disposeable within a separate one of the radially-outwardly extending 16, 18 or radially inwardly from a remainder of thecasing recesses connector 30 so as to be disposeable within a separate one of the radially-inwardly extending 16, 18. As such, thecasing recesses retainer 24 is configured to either prevent displacement of theconnector 22 in a radial direction generally toward thecasing axis 21 to maintain the 30, 32 engaged with radially-outwardly extendingconnector lugs 16, 18 or to prevent displacement of thecasing recesses connector 22 in a radial direction generally away from thecasing axis 21 to maintain the 30, 32 engaged with radially-inwardly extendingconnector lugs 16, 18.casing recesses - Preferably, the
connector 22 has a pair of angled, generally opposing contact surfaces or 34A, 34B, and thesurface sections retainer 24 includes first and second axially spaced, generally 36A, 36B each having an angled “drive”annular members 37A, 37B disposed generally against a separate one of the connector angledsurface 34A, 34B, respectively. The retainer first andcontact surfaces 36A, 36B are adjustably connected such that the twosecond members 36A, 36B are displaceable generally toward each other along theretainers members axis 21 so as to bias theconnector 24 either generally radially outwardly toward the casing 13A, 15A, or radially inwardly toward the casinginner surfaces 13B, 15B, as described in further detail below. In other embodiments, such as shown inouter surfaces FIGS. 6 and 7 , theretainer 24 includes two “overlapping” annular members 40, 42 or may include a plurality of threaded rods or fasteners 44, as shown inFIGS. 8 and 9 . - Having described the basic structure of the
coupler device 10 andcasing assembly 20 of the present invention, these and other components and/or features of the various constructions of thecoupler device 10 andcasing assembly 20 are described in greater detail below. - Referring first to
FIGS. 1-3 , in a first construction, thecoupler device 10 engages with the casing 13A, 15A, and is thus disposed within an interior chamber CC of theinner surfaces casing assembly 20. With such an arrangement, each casing recess 16, 18 extends radially outwardly from the inner 13A, 15A, respectively, of thecircumferential surface 12, 14 and eachparticular casing 30, 32 extends radially outwardly from a remainder of theconnector portion lug connector 22, with theretainer 24 being configured to prevent displacement of theconnector 22 in a radial direction R1 generally toward thecasing axis 21. - Specifically, each casing recess 16, 18 is partially defined by an angled
radial contact surface 46A, 46B, a facing 47A, 47B, and an innerradial surface circumferential surface 48A, 48B extending axially between the radial surfaces, the three surfaces 46, 47 and 48 extending circumferentially about thecasing axis 21. Each one of the two casing recessangled contact surfaces 46A, 46B face generally away from the other one of the two casing recessangled surfaces 46B, 46A, for reasons discussed below. - Further, each
connector 22 includes a generallyarcuate body 50 with two opposingaxial ends 50 a, 50 b, opposing radial ends 50 c (only one shown) and inner and outer circumferential surfaces 51A, 51B. The first and 30, 32 extend from the outer surface 5B and each preferably includes a generallysecond lugs rectangular shoulder 52 extending circumferentially between the radial ends 50 c, the twoshoulders 52 being spaced apart and each located generally adjacent to a separate one of the axial ends 50 a or 50 b. Preferably, each one of the first and second connector lugs 30, 32 has anangled drive surface 53A, 53B formed on theannular shoulder 52 and extending at least partially circumferentially about thecasing axis 21. Each one of the two lug angled drive surfaces 53A, 53B faces generally toward the other one of the two lug angled surfaces 53B, 53A, respectively. Furthermore, the first lug angledsurface 53A is disposed against the first casing recess angledcontact surface 46A and the second lug angled surface 53B is disposed against the second casing recess angled surface 46B. - With the above lug and recess structure, displacement of the
connector 22 in the radially outward direction R1 (i.e., away from the axis 21) biases the 12 a, 14 a of each one of the first andend 12, 14 generally toward thesecond casings 12 a, 14 a of the other one of the first andend 12, 14. That is, the facing angled drive surfaces 53A, 53B of thesecond casings connector body 50 slide outwardly against the angled contact surfaces 46A, 46B of the casing recesses 16, 18 so as to force or “wedge” the two casing ends 12 a, 14 a together. Also, the connector angled 34A, 34B are formed or provided on the body inner surface 51A and extend circumferentially between the body radial ends 50 c. Eachcontact surface sections 34A or 34B faces generally toward an adjacent one of the twocontact surface axial ends 50 a, 50 b, respectively, and generally away from the other 34B, 34A, respectively, for reasons described in detail below.angled surface section - Still referring to
FIGS. 1-3 , theretainer 24 of the first coupler construction has first and 36A, 36B that each include a generallysecond retainer members 54, 56, respectively. Each retainerannular body 54, 56 has an inner axial end 56 a, 56 a, an outer axial end 54 b, 56 b, an innerannular body circumferential surface 55A, 57A, and an outer 55B, 57B providing one of the angled drive surfaces 37A, 37B. The twocircumferential surface 54, 56 are arranged such that the body inner ends 56 are disposed at least generally adjacent to each other and eachannular bodies 37A, 37B faces generally toward theangled drive surface 37B, 37A on theangled surface 56, 54. The twoother retainer body 54, 56 are sized to be disposed radially inwardly of theretainer bodies connector body 50 such that the retainer first angledouter surface 37A is disposed against the connector first angledinner surface section 34A and the retainer second angledouter surface 37B is disposed against the connector second angledinner surface section 34B. As such, axial movement of the 54, 56 displaces theretainer bodies connector 12 radially, as described below. - Further, the two
54, 56 are preferably adjustably connected by a plurality of threadedretainer bodies rods 58 extending axially through thesecond body 56 and secured within thefirst body 54 and a plurality ofnuts 59 each engageable with therod 58 and contactable with the outer end 56b of thesecond body 56. Preferably, therods 58 andnuts 59 are spaced circumferentially apart on the two 54, 56, as best shown inbodies FIG. 2 . Further, rotation of eachnut 59 in a first angular direction A1 displaces each 54, 56 generally toward theretainer body 56, 54, and rotation of the nuts 59 in a second angular direction A2 enables eachother body 54, 56 to displace generally away from thebody 56, 54.other body - With the above structure, displacement of the
54, 56 axially toward each other cause each retainer angledretainer bodies 37A, 37B to slide against the associateddrive surface 34A, 34B, respectively, of theangled contact surface connectors 22 while displacing toward the 37B, 37A, which forces or wedges theother drive surface connectors 22 to displace radially outwardly. Such radial outward displacement of theconnectors 22 cause the connector lugs 30, 32 to advance into the casing recesses 16, 18 to securely connect the casing ends 12 a, 14 a, as described above. Alternatively, displacement of the 54, 56 axially away from each other cause each retainer angledretainer bodies 37A, 37B to displace away from each other, which enables thedrive surface connectors 22 to displace radially inwardly. Such radial inward displacement of theconnectors 22 cause the connector lugs 30, 32 to withdraw from the casing recesses 16, 18, thereby disconnecting the casing ends 12 a, 14 a. - Referring to
FIGS. 1 and 2 , the first construction of thecoupler device 10 also preferably comprises a generallytubular guide member 49 disposed radially inwardly of theretainer 24 and configured to generally retain theconnectors 22 disposed adjacent to the casing recesses 16, 18 during installation and removal of thecoupler device 10. Specifically, theguide member 49 at least temporarily supports the plurality ofconnectors 22 prior to insertion of the two 54, 56 between theretainer bodies guide member 49 and theconnectors 22 and after removal of the 54, 56 during casing disassembly, Referring now toretainer bodies FIGS. 4 and 5 , in a second construction of thecoupler device 10 andcasing assembly 20, thecoupler device 10 engages with the casing 13B, 15B, and is thus disposed externally of theouter surfaces 12, 14. With such an arrangement, eachcasings 16, 18 extends radially inwardly from the outercasing recess 13B, 15B, respectively, of thecircumferential surface 12, 14 and eachparticular casing 30, 32 extends radially inwardly from a remainder of theconnector portion lug connector 22, with theretainer 24 being configured to prevent displacement of theconnector 22 in a radial direction R2 generally away from thecasing axis 21. - Specifically, each
16, 18 is partially defined by an angledcasing recess 60A, 60B, a facing radial surface 61A, 61B, and an outerradial contact surface circumferential surface section 62A, 62B extending axially between the radial surfaces, the three surfaces 60, 61 and 62 extending circumferentially about thecasing axis 21. Each one of the two casing recess angled contact surfaces 60A, 60B faces generally away from the other one of the two casing recess angled surfaces 60B, 60A, for reasons discussed below. - Further, each
connector 22 includes a generallyarcuate body 64 with two opposing axial ends 64 a, 64 b, opposing radial ends 64 c, and inner and outer 65A, 65B. The first andcircumferential surfaces 30, 32 extend from the bodysecond lugs inner surface 65A and each preferably includes a generallyrectangular shoulder 66 extending circumferentially between the radial ends 64 c, the twoshoulders 64 being spaced apart and each located generally adjacent to a separate one of the axial ends 64 a or 64 b. Preferably, each one of the first and second connector lugs 30, 32 has an 68A, 68B formed on theangled drive surface annular shoulder 66 and extending at least partially circumferentially about and facing generally towards the casingaxis 21. Each one of the two lug angled drive surfaces 68A, 68B also faces generally toward the other one of the two lug angled surfaces 68B, 68A, respectively. Furthermore, the first lug angledsurface 68A is disposeable or disposed against the first casing recess angledcontact surface 60A and the second lug angledsurface 68B is disposeable/disposed against the second casing recess angledsurface 60B. - With the above lug and recess structure, displacement of the
connector 22 in the radially inward direction R2 (i.e., toward the axis 21) biases the 12 a or 14 a of each one of the first andend 12, 14 generally toward thesecond casings 12 a, 14 a of the other one of the first andend 12, 14. That is, the connector facing angled drive surfaces 68A, 68B slide inwardly against the casing recess angled contact surfaces 60A, 60B so as to force or “wedge” the two casing ends 12 a, 14 a together. Also, the connector angledsecond casings 34A, 34B are formed or provided on thecontact surface sections outer surface 65B of eachconnector body 64, extend circumferentially between the body radial ends 64 c and face generally away from thecasing axis 21. Each 34A or 34B also faces generally toward an adjacent one of the twoconnector contact surface axial ends 64 a, 64 b, respectively, and generally away from the other 34B, 34A, respectively, for reasons described in detail below.angled surface section - Still referring to
FIGS. 4 and 5 , theretainer 24 of the second coupler construction has first and 36A, 36B that each include a generallysecond retainer members 70, 72, respectively. Each retainerannular body 70, 72 has an inner axial end 70 a, 72 a, an outer axial end 70 b, 72 b, an inner circumferential surface 71A, 73A providing one of the angled drive surfaces 37A, 37B, and an outer circumferential surface 71B, 73B. The twoannular body 70, 72 are arranged such that the body inner ends 70 a, 72 a are disposed at least generally adjacent to each other and eachannular bodies 37A, 37B faces generally toward theangled drive surface 37B, 37A on theangled surface 72, 70. The twoother retainer body 70, 72 are sized to be disposed radially outwardly of theretainer bodies connector body 64, and are thus diametrically larger than the casing 13B, 15B, and are arrangeable/arranged such that the retainer first angledouter surfaces inner surface 37A is disposed against the connector first angledouter surface section 34A and the retainer second angledinner surface 37B is disposed against the connector second angledouter surface section 34B. As such, axial movement of the 70, 72 displaces theretainer bodies connector 12 radially, as described below. - Preferably, the
first retainer body 70 is generally tubular and has three sections: an outer, angled section 71 a providing theangled drive surface 37A, an inner, radially enlarged section 71 b having a plurality of “blind holes” 76 (one shown), as discussed below, and a central portion 71 c extending axially between and connecting the inner and outer sections 71 a, 71 b. Thesecond retainer body 72 is preferably formed as a generally rectangular ring with the angled drive surface 37 b extending axially entirely along the bodyinner surface 73. Further, each of the 70, 72 is preferably formed of a plurality of semicircular, partial-circular or arcuate sections (not indicated), so as to facilitate installation about theretainer bodies connectors 22, but may alternatively be provided by one-piece annular bodies or rings. - Further, the two
70, 72 are preferably adjustably connected by a plurality of threadedretainer bodies rods 74 extending axially through thesecond body 72 and secured within a separate one of theblind holes 76 of thefirst body 70 and a plurality ofnuts 75 each engaged with therod 74 and contactable with the outer end 72 b of thesecond body 72. Preferably, therods 74 and threaded openings are spaced circumferentially apart on the two 70, 72, as best shown inbodies FIG. 4 . Further, rotation of eachnut 75 in a first angular direction A1 displaces each 70, 72 generally toward theretainer body 72, 70, and rotation of the nuts 75 in a second angular direction A2 enables eachother body 70, 72 to be displaced generally away from thebody 72, 70.other body - With the above structure, displacement of the
70, 72 axially toward each other cause each retainer angledretainer bodies 37A, 37B to slide against the associateddrive surface 34A, 34B, respectively, of theangled contact surface connectors 22 while displacing toward the 37B, 37A, which forces or wedges theother drive surface connectors 22 to displace radially inwardly. Such radial inward displacement of theconnectors 22 cause the connector lugs 30, 32 to advance into the casing recesses 16, 18 to securely connect the casing ends 12 a, 14 a, as described above. Alternatively, displacement of the 70, 72 axially away from each other cause each retainer angledretainer bodies 37A, 37B to displace away from each other, which enables thedrive surface connectors 22 to displace radially outwardly. Such radial outward displacement of theconnectors 22 permits the connector lugs 30, 32 to be withdrawn from the casing recesses 16, 18, thereby disconnecting the casing ends 12 a, 14 a. - Referring now to
FIGS. 6 and 7 , in a third construction of thecoupler device 10 andcasing assembly 20, thecoupler device 10 engages with the casing 13B, 15B, and is thus disposed externally of theouter surfaces 12, 14 as with the second construction. As with the second construction, eachcasings 16, 18 extends radially inwardly from the outercasing recess 13B, 15B, respectively, of thecircumferential surface 12, 14 and eachparticular casing 30, 32 extends radially inwardly from a remainder of theconnector portion lug connector 22, with theretainer 24 being configured to prevent displacement of theconnector 22 in a radial direction R2 generally away from thecasing axis 21. - Specifically, each
16, 18 is partially defined by an angledcasing recess radial contact surface 80A, 80B, a facingradial surface 81A, 81B, and an outer 82A, 82B extending axially between the radial surfaces, the three surfaces 80, 81 and 82 extending circumferentially about thecircumferential surface section casing axis 21. Each one of the two casing recess angled contact surfaces 80A, 80B faces generally away from the other one of the two casing recess angled surfaces 80B, 80A, for reasons as discussed above with the second construction and in further detail below. - Further, each
connector 22 includes a generallyarcuate body 84 with two opposing axial ends 84 a, 84 b, opposing radial ends 84 c (only one shown) and inner and outer 85A, 85B. The first andcircumferential surfaces 30, 32 extend from the bodysecond lugs inner surface 85A and each preferably includes a generally rectangular,annular body portion 86 extending circumferentially between the radial ends 84 c, the twoannular body portions 86 being axially spaced apart and each located generally adjacent to a separate one of the axial ends 84 a or 84 b. Preferably, each one of the first and second connector lugs 30, 32 has anangled drive surface 88A, 88B formed on theannular body portion 86 and extending at least partially circumferentially about and facing generally towards the casingaxis 21. Each one of the two lug angled drive surfaces 88A, 88B also faces generally toward the other one of the two lug angled surfaces 88B, 88A, respectively. Furthermore, the first lug angledsurface 88A is disposeable or disposed against the first casing recess angledcontact surface 80A and the second lug angled surface 88B is disposeable/disposed against the second casing recess angled surface 80B. - With the above lug and recess structure, displacement of the
connector 22 in the radially inward direction R2 (i.e., toward the axis 21) biases the 12 a or 14 a of each one of the first andend 12, 14 generally toward thesecond casings 14 a, 12 a of the other one of the first andend 14, 12, in a manner generally similar with the second coupler and casing constrction. That is, the connector facing angled drive surfaces 88A, 88B slide inwardly against the casing recess angled contact surfaces 80A, 80B so as to force or “wedge” the two casing ends 12 a, 14 a together.second casings - However, in contrast with the both the first and second coupler constructions, each
connector body 84 is formed without angled contact surfaces engageable by theretainer 24. Rather, the body outercircumferential surface 85B is substantially “radially constant”, i.e., the body outside radius does not vary on theouter surface 85B. - Still referring to
FIGS. 6 and 7 , theretainer 24 of the third coupler construction has first and 36A, 36B that include inner and outer generallysecond retainer members 90, 92, respectively. Each generally annularannular members 90, 92 has an opposing axial ends 90 a, 92 a, an innermember 91A, 93A and an outer circumferential surface 91B, 93B, respectively. Thecircumferential surface inner member 90 is disposed generally between theconnector body 84 and theouter member 92 such that the inner memberinner surface 91A is disposed against the connector bodyouter surface 85B and the inner member outer surface 91B is disposed against the outer memberinner surface 93A. Further, the inner member outer surface 91B and the outer memberinner surface 93A are each generally angled and arranged such that eachsurface 91B, 93A faces generally toward theother surface 93A, 91B and are juxtaposeable against each other. - With this structure, axial displacement of the
outer member 92 relative to theinner member 90 in a first axial direction D1 biases theinner member 90 generally radially inwardly toward theconnector 22. That is, as theouter body 92 displaces axially in the first direction D1, the outer bodyinner surface 93A, slides against the inner body outer surface 91B and forces theinner body 90 to displace or at least compress radially inwardly. Thereby, theinner member 90 exerts a radially inwardly directed force F on theconnector 22 such that the connector lug drive surfaces 88A, 88B slide along or are at least biased against, the casing recess contact surfaces 80A, 80B as discussed above. Alternatively, axial displacement of theouter member 92 relative to theinner member 90 in a second, opposing axial direction D2 removes the radially-inwardly directed compressive force on theinner body 90, thereby permitting removal of theinner body 90 and thereafter theconnector 22 so as to disengage the 30, 32 from the casing recesses 16, 18.lugs - Referring to
FIGS. 8 and 9 , in a fourth construction of thecoupler device 10 andcasing assembly 20, thecoupler device 10 is disposed externally of the 12, 14 and engages with the casingcasings 13B, 15B, as with the second and third constructions. Thus, eachouter surfaces 16, 18 extends radially inwardly from the outercasing recess 13B, 15B, respectively, of thecircumferential surface 12, 14, eachparticular casing 30, 32 extends radially inwardly from a remainder of theconnector portion lug connector 22, and theretainer 24 is configured to prevent displacement of theconnector 22 in a radial direction R2 generally away from thecasing axis 21. - Specifically, each
16, 18 is partially defined by an angledcasing recess 100A, 100B, a facingradial contact surface radial surface 101A, 101B, and an outercircumferential surface section 102A, 102B extending axially between the radial surfaces, the three surfaces 100, 101 and 102 extending circumferentially about thecasing axis 21. Each one of the two casing recess angled contact surfaces 100A, 100B faces generally away from the other one of the two casing recess angled surfaces 100B, 100A, so as to engage with complementary lug drive surfaces 108, 108B in a manner discussed below. - Further, each
connector 22 includes a generallyrectangular bar 104 having opposing axial ends 104 a, 104 b, opposing radial ends 104 c and inner and 105A, 105B. Eachouter surfaces rectangular bar 104 is sized substantially “circumferentially smaller”, i.e., has a much lesser circumferential extent, in comparison with the 50, 64, 84 of the first, second, and third constructions, respectively. As such, the fourth construction has a greater number of theconnector bodies connectors 22 in comparison with the previously described constructions. - Further, the first and second connector lugs 30, 32 extend from the body
inner surface 105A and each preferably includes a generallyrectangular body portion 106 extending circumferentially between the radial ends 104 c, the twoannular body portions 106 being axially spaced apart and each located generally adjacent to a separate one of the axial ends 104 a or 104 b. Preferably, each one of the first and second connector lugs 30, 32 has an angled drive surface 108A, 108B formed on therectangular body portion 106 and extending at least partially circumferentially about and facing generally towards the casingaxis 21. Each one of the two lug angled drive surfaces 108A, 108B also faces generally toward the other one of the two lug angled surfaces 108B, 108A, respectively. Furthermore, the first lug angled surface 108A is disposeable or disposed against the first casing recess angledcontact surface 100A and the second lug angled surface 108B is disposeable/disposed against the second casing recess angledsurface 100B. Thus, displacement of theconnector 22 in the radially inward direction R2 (i.e., toward the axis 21) biases the 12 a or 14 a of each one of the first andend 12, 14 generally toward thesecond casings 12 a, 14 a of the other one of the first andend 12, 14, in a manner generally similar with the second and third coupler and casing constructions.second casings - As best shown in
FIG. 8 , the fourth construction of thecoupler device 10 preferably includes a plurality ofretainers 24, most preferably tworetainers 24 for eachconnector 22. Specifically, eachretainer 24 preferably includes a threaded rod orfastener 110 and anut 112 engageable with therod 110. Eachrod 110 has a first end 110 a connected with the one of the 12, 14 and a second end 110 b extending outwardly of thecasings connector body 84, the second end 110 b being threaded so as to be engageable by the nut. As such, eachnut 112 clamps against the connector bodyouter surface 105B, so as to force the connector lugs 30, 32 to displace radially inwardly to connect the casing ends 12 a, 14 a. - It will be appreciated by those skilled in the art that changes could be made to the embodiments described above without departing from the broad inventive concept thereof It is understood, therefore, that this invention is not limited to the particular embodiments disclosed, but it is intended to cover modifications within the spirit and scope of the present invention as generally defined in the appended claims.
Claims (27)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/215,184 US7922218B2 (en) | 2008-06-25 | 2008-06-25 | Shear ring casing coupler device |
| BRPI0901998-7A BRPI0901998A2 (en) | 2008-06-25 | 2009-06-24 | shear ring casing coupling device |
| US13/010,465 US8430433B2 (en) | 2008-06-25 | 2011-01-20 | Shear ring casing coupler device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/215,184 US7922218B2 (en) | 2008-06-25 | 2008-06-25 | Shear ring casing coupler device |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US13/010,465 Continuation US8430433B2 (en) | 2008-06-25 | 2011-01-20 | Shear ring casing coupler device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| US20090324404A1 true US20090324404A1 (en) | 2009-12-31 |
| US7922218B2 US7922218B2 (en) | 2011-04-12 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US12/215,184 Expired - Fee Related US7922218B2 (en) | 2008-06-25 | 2008-06-25 | Shear ring casing coupler device |
| US13/010,465 Expired - Fee Related US8430433B2 (en) | 2008-06-25 | 2011-01-20 | Shear ring casing coupler device |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US13/010,465 Expired - Fee Related US8430433B2 (en) | 2008-06-25 | 2011-01-20 | Shear ring casing coupler device |
Country Status (2)
| Country | Link |
|---|---|
| US (2) | US7922218B2 (en) |
| BR (1) | BRPI0901998A2 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100270308A1 (en) * | 2009-04-22 | 2010-10-28 | Hitachi Plant Technologies, Ltd. | End wall closure apparatus |
| US11085373B2 (en) * | 2019-01-31 | 2021-08-10 | Rolls-Royce North American Technologies Inc. | Gas turbine engine with mount for interchangeable inlets |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BR112014007313B1 (en) * | 2011-09-27 | 2020-11-17 | Dresser-Rand Company | COMPRESSION SYSTEM AND METHOD FOR SUPPORTING A COMPRESSION SYSTEM WITHOUT A BASE PLATE |
| US8740260B1 (en) * | 2012-12-04 | 2014-06-03 | Vetco Gray Inc. | Rapid make up drive screw adapter |
| EP2999908B1 (en) * | 2013-05-22 | 2018-05-09 | National Oilwell Varco Norway AS | Coupler device and method for using the same |
| NO341357B1 (en) * | 2015-08-26 | 2017-10-23 | Aker Solutions As | Clamp connector |
| US10400925B2 (en) * | 2016-04-08 | 2019-09-03 | Axon Pressure Products, Inc. | Manual quick connect hub clamping system |
| US10619782B2 (en) * | 2018-03-23 | 2020-04-14 | Kennedy Valve Company | Breaker clamp for fire hydrant |
| RU2703583C1 (en) * | 2019-03-27 | 2019-10-21 | Общество с ограниченной ответственностью "Газпром 335" | Flange connector |
| RU2720144C1 (en) * | 2019-06-14 | 2020-04-24 | Общество с ограниченной ответственностью "Газпром 335" | Flange rotary joint |
| US11802641B2 (en) * | 2019-10-07 | 2023-10-31 | Gartech, Llc | Clamp with jaw assembly and method of use |
| NO347425B1 (en) * | 2021-06-17 | 2023-10-30 | Aquamarine As | A clamp and a method of clamping a pair of flanges |
Citations (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1622768A (en) * | 1924-06-04 | 1927-03-29 | Cook Henry Denman | Pipe joint and connection |
| US2328031A (en) * | 1941-06-27 | 1943-08-31 | Dresser Mfg Company | Pipe clamp and method and apparatus for applying same |
| US2836117A (en) * | 1954-07-06 | 1958-05-27 | Harry G Lankford | Clamp means |
| US2868565A (en) * | 1956-05-01 | 1959-01-13 | George E Suderow | Releasable pivoted clamp for joining internally flanged structural members |
| US3044657A (en) * | 1957-06-14 | 1962-07-17 | Richard H Horton | Flange and wall structure |
| US3220245A (en) * | 1963-03-25 | 1965-11-30 | Baker Oil Tools Inc | Remotely operated underwater connection apparatus |
| US3352577A (en) * | 1967-06-27 | 1967-11-14 | Koppers Co Inc | Coupling arrangement for filament reinforced thermosetting resin tubular members |
| US3628812A (en) * | 1969-12-01 | 1971-12-21 | Exxon Production Research Co | Removable pipe connector |
| US4146261A (en) * | 1977-02-12 | 1979-03-27 | Motoren- Und Turbinen-Union Friedrichshafen Gmbh | Clamping arrangement |
| US4205927A (en) * | 1977-12-16 | 1980-06-03 | Rolls-Royce Limited | Flanged joint structure for composite materials |
| US4573527A (en) * | 1983-07-29 | 1986-03-04 | Mcdonough M J | Heat exchanger closure connection |
| US4984830A (en) * | 1988-11-02 | 1991-01-15 | Cooper Industries, Inc. | Collet type connector |
| US5024585A (en) * | 1990-04-09 | 1991-06-18 | Sta-Rite Industries, Inc. | Housing coupling mechanism |
| US5443581A (en) * | 1992-12-03 | 1995-08-22 | Wood George & Co., Inc. | Clamp assembly for clamp hub connectors and a method of installing the same |
| US5951066A (en) * | 1998-02-23 | 1999-09-14 | Erc Industries, Inc. | Connecting system for wellhead components |
| US5967746A (en) * | 1997-07-30 | 1999-10-19 | Mitsubishi Heavy Industries, Ltd. | Gas turbine interstage portion seal device |
| US6123363A (en) * | 1998-11-02 | 2000-09-26 | Uop Llc | Self-centering low profile connection with trapped gasket |
| US6467988B1 (en) * | 2000-05-20 | 2002-10-22 | General Electric Company | Reducing cracking adjacent shell flange connecting bolts |
| US6658986B2 (en) * | 2002-04-11 | 2003-12-09 | Visteon Global Technologies, Inc. | Compressor housing with clamp |
| US6688802B2 (en) * | 2001-09-10 | 2004-02-10 | Siemens Westinghouse Power Corporation | Shrunk on industrial coupling without keys for industrial system and associated methods |
| US6715802B2 (en) * | 1999-10-18 | 2004-04-06 | William J. Baker | Apparatus for connecting tubular bodies |
| US6764284B2 (en) * | 2002-01-10 | 2004-07-20 | Parker-Hannifin Corporation | Pump mount using sanitary flange clamp |
| US6824171B2 (en) * | 2002-08-23 | 2004-11-30 | Dril-Quip, Inc. | Riser connector |
| US7481464B2 (en) * | 2006-06-08 | 2009-01-27 | Karl Hamacher Gmbh | Coupling, particularly pipe coupling for high-pressure pipes or hoses |
| US7527306B2 (en) * | 2002-05-30 | 2009-05-05 | Arkal Filtration Systems C.S. Ltd. | Pipe coupling |
Family Cites Families (323)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US815812A (en) * | 1904-08-01 | 1906-03-20 | George Westinghouse | Gas-purifying apparatus. |
| US1061656A (en) * | 1906-02-19 | 1913-05-13 | Joseph L Black | Separator for mechanical mixtures of gases. |
| US1057613A (en) * | 1910-11-01 | 1913-04-01 | William J Baldwin | Art of separating materials from gases. |
| US1480775A (en) * | 1923-01-05 | 1924-01-15 | Nicholas C Marien | Air washer |
| US1642454A (en) * | 1926-05-19 | 1927-09-13 | Vaino W Malmstrom | Pump, compressor, or the like |
| US2006244A (en) * | 1933-07-10 | 1935-06-25 | Julius F Kopsa | Liquid-separating device |
| US2300766A (en) * | 1940-05-10 | 1942-11-03 | Bbc Brown Boveri & Cie | Multistage centrifugal compressor |
| US2345437A (en) * | 1943-07-09 | 1944-03-28 | Nat Tube Co | Thrust bearing |
| US2811303A (en) * | 1948-12-28 | 1957-10-29 | Joy Mfg Co | Impeller for axial flow fans |
| US2602462A (en) * | 1950-12-12 | 1952-07-08 | Ralph A Barrett | Condensate unloader valve |
| US2932360A (en) * | 1956-04-02 | 1960-04-12 | Carrier Corp | Apparatus for treating air |
| US2954841A (en) * | 1956-11-16 | 1960-10-04 | Jersey Prod Res Co | Centrifugal separator |
| US2897917A (en) * | 1957-11-15 | 1959-08-04 | Fairchild Engine & Airplane | Apparatus for separating moisture and condensable vapors from a gas |
| US3213794A (en) * | 1962-02-02 | 1965-10-26 | Nash Engineering Co | Centrifugal pump with gas separation means |
| US3191364A (en) * | 1962-05-28 | 1965-06-29 | American Air Filter Co | Centrifugal dust separator |
| NL299872A (en) * | 1962-10-30 | 1900-01-01 | ||
| US3273325A (en) * | 1963-01-09 | 1966-09-20 | Universal Oil Prod Co | Rotary gas separator |
| US3204696A (en) * | 1963-09-16 | 1965-09-07 | California Research Corp | Apparatus for exhausting from downhole burner |
| US3395511A (en) * | 1963-10-03 | 1968-08-06 | Atlas Copco Ab | Method and means for obtaining dry gas or air |
| US3402434A (en) * | 1965-12-22 | 1968-09-24 | Om Ltd | Drawing frame for high speed operation |
| US3431747A (en) | 1966-12-01 | 1969-03-11 | Hadi T Hashemi | Engine for exchanging energy between high and low pressure systems |
| US3420434A (en) | 1966-12-30 | 1969-01-07 | Judson S Swearingen | Rotary compressors and systems employing same using compressor gas as seal gas |
| DK117925B (en) * | 1967-03-09 | 1970-06-15 | Grundfos As | Adapter for a submersible pump set. |
| US3399773A (en) * | 1967-04-14 | 1968-09-03 | Read Ivan Jay | Apparatus for separating solids from liquids |
| US3490209A (en) * | 1968-02-20 | 1970-01-20 | United Aircraft Prod | Liquid separator |
| US3578342A (en) * | 1969-01-14 | 1971-05-11 | Satterthwaite James G | Shaft seal |
| US3500614A (en) * | 1969-02-10 | 1970-03-17 | Univ Illinois | Electro-aerodynamic precipitator |
| GB1302044A (en) * | 1969-04-10 | 1973-01-04 | ||
| SE340547B (en) * | 1970-03-02 | 1971-11-22 | Skf Svenska Kullagerfab Ab | |
| DE2138474A1 (en) * | 1971-07-31 | 1973-02-08 | Skf Kugellagerfabriken Gmbh | HYDROSTATIC AXIAL BEARING |
| JPS5224186B2 (en) * | 1972-03-03 | 1977-06-29 | ||
| GB1484994A (en) * | 1973-09-03 | 1977-09-08 | Svenska Rotor Maskiner Ab | Shaft seal system for screw compressors |
| US4117359A (en) * | 1974-01-30 | 1978-09-26 | Teldix Gmbh | Bearing and drive structure for spinning turbine |
| US4112687A (en) * | 1975-09-16 | 1978-09-12 | William Paul Dixon | Power source for subsea oil wells |
| US4103899A (en) * | 1975-10-01 | 1978-08-01 | United Technologies Corporation | Rotary seal with pressurized air directed at fluid approaching the seal |
| US4033647A (en) * | 1976-03-04 | 1977-07-05 | Borg-Warner Corporation | Tandem thrust bearing |
| US4165622A (en) * | 1976-04-30 | 1979-08-28 | Bourns, Inc. | Releasable locking and sealing assembly |
| US4059364A (en) * | 1976-05-20 | 1977-11-22 | Kobe, Inc. | Pitot compressor with liquid separator |
| NL7607039A (en) * | 1976-06-28 | 1977-12-30 | Ultra Centrifuge Nederland Nv | CENTRIFUGE FOR THE SEPARATION OF HELIUM FROM NATURAL GAS. |
| US4087261A (en) * | 1976-08-30 | 1978-05-02 | Biphase Engines, Inc. | Multi-phase separator |
| US4078809A (en) * | 1977-01-17 | 1978-03-14 | Carrier Corporation | Shaft seal assembly for a rotary machine |
| US4174925A (en) * | 1977-06-24 | 1979-11-20 | Cedomir M. Sliepcevich | Apparatus for exchanging energy between high and low pressure systems |
| US4141283A (en) * | 1977-08-01 | 1979-02-27 | International Harvester Company | Pump unloading valve for use in agricultural tractor lift systems |
| US4135542A (en) * | 1977-09-12 | 1979-01-23 | Chisholm James R | Drain device for compressed air lines |
| EP0004145B1 (en) * | 1978-02-28 | 1984-07-11 | Fred Mellor | Fluid/particle separator unit |
| US4384724A (en) * | 1978-08-17 | 1983-05-24 | Derman Karl G E | Sealing device |
| US4197990A (en) * | 1978-08-28 | 1980-04-15 | General Electric Company | Electronic drain system |
| US4333748A (en) * | 1978-09-05 | 1982-06-08 | Baker International Corporation | Rotary gas/liquid separator |
| DE2842967C2 (en) * | 1978-10-02 | 1984-08-16 | Westfalia Separator Ag, 4740 Oelde | Continuously operating drum for concentrating suspended solids |
| US4259045A (en) * | 1978-11-24 | 1981-03-31 | Kayabakogyokabushikikaisha | Gear pump or motor units with sleeve coupling for shafts |
| US4227373A (en) * | 1978-11-27 | 1980-10-14 | Biphase Energy Systems, Inc. | Waste heat recovery cycle for producing power and fresh water |
| AT359941B (en) * | 1979-01-18 | 1980-12-10 | Buchelt Benno | WATER TURBINE |
| US4396361A (en) * | 1979-01-31 | 1983-08-02 | Carrier Corporation | Separation of lubricating oil from refrigerant gas in a reciprocating compressor |
| US4258551A (en) * | 1979-03-05 | 1981-03-31 | Biphase Energy Systems | Multi-stage, wet steam turbine |
| US4441322A (en) * | 1979-03-05 | 1984-04-10 | Transamerica Delaval Inc. | Multi-stage, wet steam turbine |
| US4298311A (en) * | 1980-01-17 | 1981-11-03 | Biphase Energy Systems | Two-phase reaction turbine |
| US4339923A (en) * | 1980-04-01 | 1982-07-20 | Biphase Energy Systems | Scoop for removing fluid from rotating surface of two-phase reaction turbine |
| US4336693A (en) * | 1980-05-01 | 1982-06-29 | Research-Cottrell Technologies Inc. | Refrigeration process using two-phase turbine |
| US4438638A (en) * | 1980-05-01 | 1984-03-27 | Biphase Energy Systems | Refrigeration process using two-phase turbine |
| US4375975A (en) * | 1980-06-04 | 1983-03-08 | Mgi International Inc. | Centrifugal separator |
| US4347900A (en) * | 1980-06-13 | 1982-09-07 | Halliburton Company | Hydraulic connector apparatus and method |
| JPS612832Y2 (en) * | 1980-09-12 | 1986-01-29 | ||
| US4334592A (en) * | 1980-12-04 | 1982-06-15 | Conoco Inc. | Sea water hydraulic fluid system for an underground vibrator |
| US4374583A (en) * | 1981-01-15 | 1983-02-22 | Halliburton Company | Sleeve valve |
| US4432470A (en) * | 1981-01-21 | 1984-02-21 | Otto Engineering, Inc. | Multicomponent liquid mixing and dispensing assembly |
| US4471795A (en) * | 1981-03-06 | 1984-09-18 | Linhardt Hans D | Contamination free method and apparatus for transfer of pressure energy between fluids |
| US4363608A (en) * | 1981-04-20 | 1982-12-14 | Borg-Warner Corporation | Thrust bearing arrangement |
| US4391102A (en) * | 1981-08-10 | 1983-07-05 | Biphase Energy Systems | Fresh water production from power plant waste heat |
| US4463567A (en) * | 1982-02-16 | 1984-08-07 | Transamerica Delaval Inc. | Power production with two-phase expansion through vapor dome |
| US4453893A (en) * | 1982-04-14 | 1984-06-12 | Hutmaker Marlin L | Drainage control for compressed air system |
| US4477223A (en) * | 1982-06-11 | 1984-10-16 | Texas Turbine, Inc. | Sealing system for a turboexpander compressor |
| US4502839A (en) * | 1982-11-02 | 1985-03-05 | Transamerica Delaval Inc. | Vibration damping of rotor carrying liquid ring |
| US4511309A (en) * | 1983-01-10 | 1985-04-16 | Transamerica Delaval Inc. | Vibration damped asymmetric rotor carrying liquid ring or rings |
| US4832709A (en) * | 1983-04-15 | 1989-05-23 | Allied Signal, Inc. | Rotary separator with a bladeless intermediate portion |
| US4541531A (en) * | 1983-08-04 | 1985-09-17 | Laros Equipment Company | Rotary separator |
| DE3336345A1 (en) * | 1983-10-06 | 1985-04-18 | Gebr. Eickhoff Maschinenfabrik U. Eisengiesserei Mbh, 4630 Bochum | HIGH PRESSURE BALL VALVE |
| US4536134A (en) * | 1984-04-30 | 1985-08-20 | Hi-Tech Engineering, Inc. | Piston seal access apparatus |
| US4574815A (en) * | 1984-08-29 | 1986-03-11 | Deere & Company | Rotor for an axial flow rotary separator |
| US4648806A (en) * | 1985-06-12 | 1987-03-10 | Combustion Engineering, Inc. | Gas compressor |
| US4687017A (en) * | 1986-04-28 | 1987-08-18 | Nupro Company | Inverted bellows valve |
| GB2192238B (en) * | 1986-07-02 | 1990-05-23 | Rolls Royce Plc | Gas turbine engine power turbine |
| DE3768172D1 (en) * | 1986-07-07 | 1991-04-04 | Diesel Kiki Co | SLIDE VALVE COMPRESSOR WITH VARIABLE FLOW RATE. |
| US4807664A (en) * | 1986-07-28 | 1989-02-28 | Ansan Industries Ltd. | Programmable flow control valve unit |
| US4821737A (en) * | 1986-08-25 | 1989-04-18 | The Boc Group, Inc. | Water separator |
| US4813495A (en) * | 1987-05-05 | 1989-03-21 | Conoco Inc. | Method and apparatus for deepwater drilling |
| US4752185A (en) * | 1987-08-03 | 1988-06-21 | General Electric Company | Non-contacting flowpath seal |
| JPH01207151A (en) | 1988-02-16 | 1989-08-21 | Mitsubishi Heavy Ind Ltd | Centrifugal gas-liquid separator |
| US4830331A (en) * | 1988-07-22 | 1989-05-16 | Vindum Jorgen O | High pressure fluid valve |
| JPH02274605A (en) | 1989-04-14 | 1990-11-08 | Topy Ind Ltd | Elastic body device |
| US5202024A (en) | 1989-06-13 | 1993-04-13 | Alfa-Laval Separation Ab | Centrifugal separator |
| GB2235246A (en) | 1989-06-20 | 1991-02-27 | Epic Prod Ltd | A drive system for a pump/compressor |
| US5007328A (en) | 1989-07-24 | 1991-04-16 | Otteman John H | Linear actuator |
| US5054995A (en) | 1989-11-06 | 1991-10-08 | Ingersoll-Rand Company | Apparatus for controlling a fluid compression system |
| JPH03185285A (en) | 1989-12-15 | 1991-08-13 | Mitsubishi Oil Co Ltd | Rotary liquid flow pump with gas removal function |
| JPH0433431Y2 (en) | 1990-05-23 | 1992-08-11 | ||
| US5045046A (en) | 1990-11-13 | 1991-09-03 | Bond Lesley O | Apparatus for oil separation and recovery |
| US5080137A (en) | 1990-12-07 | 1992-01-14 | Adams Thomas R | Vortex flow regulators for storm sewer catch basins |
| US5211427A (en) | 1990-12-22 | 1993-05-18 | Usui Kokusai Sangyo Kaisha Ltd. | Piping connector |
| US5190440A (en) | 1991-03-11 | 1993-03-02 | Dresser-Rand Company | Swirl control labyrinth seal |
| US5207810A (en) | 1991-04-24 | 1993-05-04 | Baker Hughes Incorporated | Submersible well pump gas separator |
| DE4137633A1 (en) | 1991-11-15 | 1993-05-19 | Nied Roland | WINDSHIELD AND METHOD FOR OPERATING A WINDSHIELD |
| US5306051A (en) | 1992-03-10 | 1994-04-26 | Hydrasearch Co., Inc. | Self-aligning and self-tightening hose coupling and method therefor |
| US5202026A (en) | 1992-04-03 | 1993-04-13 | The United States Of America As Represented By The Secretary Of The Navy | Combined centrifugal force/gravity gas/liquid separator system |
| US5203891A (en) | 1992-04-03 | 1993-04-20 | The United States Of America As Represented By The Secretary Of The Navy | Gas/liquid separator |
| JPH0767253B2 (en) | 1992-04-06 | 1995-07-19 | 動力炉・核燃料開発事業団 | Turbine generator |
| US5385446A (en) | 1992-05-05 | 1995-01-31 | Hays; Lance G. | Hybrid two-phase turbine |
| US5664420A (en) | 1992-05-05 | 1997-09-09 | Biphase Energy Company | Multistage two-phase turbine |
| SE510561C2 (en) | 1992-06-30 | 1999-06-07 | Cyclotech Ab | Centrifugal separator |
| DE9308085U1 (en) | 1992-06-30 | 1993-08-05 | Nill, Werner, Winterthur | Device for delayed drainage of meteor or rain water |
| US5246346A (en) | 1992-08-28 | 1993-09-21 | Tri-Line Corporation | Hydraulic power supply |
| SE502099C2 (en) | 1992-12-21 | 1995-08-14 | Svenska Rotor Maskiner Ab | screw compressor with shaft seal |
| US5628623A (en) | 1993-02-12 | 1997-05-13 | Skaggs; Bill D. | Fluid jet ejector and ejection method |
| GB9306980D0 (en) | 1993-04-03 | 1993-05-26 | Blp Components Ltd | Solenoid valves |
| JP2786581B2 (en) | 1993-07-23 | 1998-08-13 | 三菱重工業株式会社 | Gas-liquid separation device |
| US5378121A (en) | 1993-07-28 | 1995-01-03 | Hackett; William F. | Pump with fluid bearing |
| US7527598B2 (en) | 1993-08-13 | 2009-05-05 | Thermal Technologies, Inc. | Blood flow monitor with venous and arterial sensors |
| GB9317889D0 (en) | 1993-08-27 | 1993-10-13 | Vortoil Separation Systems Ltd | Fluid control |
| US5687249A (en) | 1993-09-06 | 1997-11-11 | Nippon Telephone And Telegraph | Method and apparatus for extracting features of moving objects |
| US5421708A (en) | 1994-02-16 | 1995-06-06 | Alliance Compressors Inc. | Oil separation and bearing lubrication in a high side co-rotating scroll compressor |
| DE4436879B4 (en) | 1994-03-19 | 2007-10-18 | Kaco Gmbh + Co | sealing unit |
| US5484521A (en) | 1994-03-29 | 1996-01-16 | United Technologies Corporation | Rotary drum fluid/liquid separator with energy recovery means |
| SE502682C2 (en) | 1994-04-21 | 1995-12-11 | Tetra Laval Holdings & Finance | Centrifugal separator discharge means |
| DE4415341A1 (en) | 1994-05-02 | 1995-11-09 | Teves Gmbh Alfred | Closing device for closing pressure-carrying channels in a housing |
| AT401281B (en) | 1994-05-11 | 1996-07-25 | Hoerbiger Ventilwerke Ag | LIFTING GRIPPERS |
| IT235089Y1 (en) | 1994-07-14 | 2000-03-31 | Metro International S R L | CYCLONE STEAM SEPARATOR |
| US5531811A (en) | 1994-08-16 | 1996-07-02 | Marathon Oil Company | Method for recovering entrained liquid from natural gas |
| US5525146A (en) | 1994-11-01 | 1996-06-11 | Camco International Inc. | Rotary gas separator |
| US5628912A (en) | 1994-12-14 | 1997-05-13 | Nth, Inc. | Rotary separator method for manure slurries |
| US6227379B1 (en) | 1994-12-14 | 2001-05-08 | Nth, Inc. | Rotary separator apparatus and method |
| DE29500744U1 (en) | 1995-01-18 | 1996-05-15 | Sihi Ind Consult Gmbh | Fluid machine with relief piston |
| JP3408005B2 (en) | 1995-01-30 | 2003-05-19 | 三洋電機株式会社 | Multi-cylinder rotary compressor |
| SE503978C2 (en) | 1995-03-10 | 1996-10-14 | Kvaerner Hymac As | fractionator |
| US5683235A (en) | 1995-03-28 | 1997-11-04 | Dresser-Rand Company | Head port sealing gasket for a compressor |
| US5542831A (en) | 1995-05-04 | 1996-08-06 | Carrier Corporation | Twin cylinder rotary compressor |
| US5640472A (en) | 1995-06-07 | 1997-06-17 | United Technologies Corporation | Fiber optic sensor for magnetic bearings |
| US6059539A (en) | 1995-12-05 | 2000-05-09 | Westinghouse Government Services Company Llc | Sub-sea pumping system and associated method including pressure compensating arrangement for cooling and lubricating |
| US5795135A (en) | 1995-12-05 | 1998-08-18 | Westinghouse Electric Corp. | Sub-sea pumping system and an associated method including pressure compensating arrangement for cooling and lubricating fluid |
| US5693125A (en) | 1995-12-22 | 1997-12-02 | United Technologies Corporation | Liquid-gas separator |
| US6312021B1 (en) | 1996-01-26 | 2001-11-06 | Tru-Flex Metal Hose Corp. | End-slotted flexible metal hose |
| US5664759A (en) | 1996-02-21 | 1997-09-09 | Aeroquip Corporation | Valved coupling for ultra high purity gas distribution systems |
| US5682759A (en) | 1996-02-27 | 1997-11-04 | Hays; Lance Gregory | Two phase nozzle equipped with flow divider |
| DE19608142B4 (en) | 1996-03-04 | 2013-10-10 | Hosokawa Alpine Ag | cyclone separator |
| US5750040A (en) | 1996-05-30 | 1998-05-12 | Biphase Energy Company | Three-phase rotary separator |
| US6090299A (en) | 1996-05-30 | 2000-07-18 | Biphase Energy Company | Three-phase rotary separator |
| US5685691A (en) | 1996-07-01 | 1997-11-11 | Biphase Energy Company | Movable inlet gas barrier for a free surface liquid scoop |
| GB9614257D0 (en) | 1996-07-06 | 1996-09-04 | Kvaerner Process Systems As | A pressure vessel for a cyclone |
| US5850857A (en) | 1996-07-22 | 1998-12-22 | Simpson; W. Dwain | Automatic pressure correcting vapor collection system |
| EP0826425A1 (en) | 1996-09-02 | 1998-03-04 | Shell Internationale Researchmaatschappij B.V. | Cyclone separator |
| US5899435A (en) | 1996-09-13 | 1999-05-04 | Westinghouse Air Brake Co. | Molded rubber valve seal for use in predetermined type valves, such as, a check valve in a regenerative desiccant air dryer |
| US5703424A (en) | 1996-09-16 | 1997-12-30 | Mechanical Technology Inc. | Bias current control circuit |
| JP3425308B2 (en) | 1996-09-17 | 2003-07-14 | 株式会社 日立インダストリイズ | Multistage compressor |
| GB2317128B (en) | 1996-09-17 | 2000-07-12 | Glacier Metal Co Ltd | Centrifugal separation apparatus |
| GB2323639B (en) | 1996-12-13 | 2000-08-23 | Knorr Bremse Systeme | Improvements relating to gas compressors |
| US5709528A (en) | 1996-12-19 | 1998-01-20 | Varian Associates, Inc. | Turbomolecular vacuum pumps with low susceptiblity to particulate buildup |
| JP2000511824A (en) | 1997-04-01 | 2000-09-12 | コーニンクレッカ フィリップス エレクトロニクス エヌ ヴィ | Separation device provided with cyclone chamber having centrifugal unit and vacuum cleaner provided with this separation device |
| JP3952321B2 (en) | 1997-04-07 | 2007-08-01 | Smc株式会社 | Suck back valve |
| DE69819290T2 (en) | 1997-06-20 | 2004-07-29 | Mitsubishi Heavy Industries, Ltd. | AIR SEPARATOR FOR GAS TURBINES |
| US5938819A (en) | 1997-06-25 | 1999-08-17 | Gas Separation Technology Llc | Bulk separation of carbon dioxide from methane using natural clinoptilolite |
| GB9817073D0 (en) | 1997-11-04 | 1998-10-07 | Bhr Group Ltd | Phase separator |
| GB9817071D0 (en) | 1997-11-04 | 1998-10-07 | Bhr Group Ltd | Cyclone separator |
| FR2771029B1 (en) | 1997-11-18 | 2000-01-28 | Total Sa | DEVICE FOR SEPARATING THE CONSTITUENTS OF A HETEROGENEOUS MIXTURE |
| FR2774136B1 (en) | 1998-01-28 | 2000-02-25 | Inst Francais Du Petrole | SINGLE SHAFT COMPRESSION-PUMP DEVICE ASSOCIATED WITH A SEPARATOR |
| US6035934A (en) | 1998-02-24 | 2000-03-14 | Atlantic Richfield Company | Method and system for separating and injecting gas in a wellbore |
| GB9803742D0 (en) | 1998-02-24 | 1998-04-15 | Kvaerner Oil & Gas As | Energy recovery |
| DE19811090A1 (en) | 1998-03-13 | 1999-09-16 | Georg Klas | Cyclone separator for effluent household gray water |
| US6145844A (en) | 1998-05-13 | 2000-11-14 | Dresser-Rand Company | Self-aligning sealing assembly for a rotating shaft |
| US5971907A (en) | 1998-05-19 | 1999-10-26 | Bp Amoco Corporation | Continuous centrifugal separator with tapered internal feed distributor |
| US5971702A (en) | 1998-06-03 | 1999-10-26 | Dresser-Rand Company | Adjustable compressor bundle insertion and removal system |
| DE19825206A1 (en) | 1998-06-05 | 1999-12-09 | Kloeckner Humboldt Wedag | Cyclone separator |
| US6068447A (en) | 1998-06-30 | 2000-05-30 | Standard Pneumatic Products, Inc. | Semi-automatic compressor controller and method of controlling a compressor |
| US6277278B1 (en) | 1998-08-19 | 2001-08-21 | G.B.D. Corp. | Cyclone separator having a variable longitudinal profile |
| US6113675A (en) | 1998-10-16 | 2000-09-05 | Camco International, Inc. | Gas separator having a low rotating mass |
| WO2000028190A1 (en) | 1998-11-11 | 2000-05-18 | Siemens Aktiengesellschaft | Shaft bearing for a turbo-machine, turbo-machine and method for operating a turbo-machine |
| EP1008759A1 (en) | 1998-12-10 | 2000-06-14 | Dresser Rand S.A | Gas compressor |
| US6217637B1 (en) | 1999-03-10 | 2001-04-17 | Jerry L. Toney | Multiple stage high efficiency rotary filter system |
| DE29906470U1 (en) | 1999-04-12 | 1999-07-29 | Konzett, Alfred, Patsch | Discharge element for a centrifugal separator |
| US6802881B2 (en) | 1999-05-21 | 2004-10-12 | Vortex Hc, Llc | Rotating wave dust separator |
| US6595753B1 (en) | 1999-05-21 | 2003-07-22 | A. Vortex Holding Company | Vortex attractor |
| US6719830B2 (en) | 1999-05-21 | 2004-04-13 | Vortex Holding Company | Toroidal vortex vacuum cleaner centrifugal dust separator |
| US20030136094A1 (en) | 1999-05-21 | 2003-07-24 | Lewis Illingworth | Axial flow centrifugal dust separator |
| US6149825A (en) | 1999-07-12 | 2000-11-21 | Gargas; Joseph | Tubular vortex separator |
| EP1074746B1 (en) | 1999-07-16 | 2005-05-18 | Man Turbo Ag | Turbo compressor |
| US6530484B1 (en) | 1999-11-18 | 2003-03-11 | Multotec Process Equipment (Proprietary) Ltd. | Dense medium cyclone separator |
| GB2358202A (en) | 2000-01-12 | 2001-07-18 | Mentor Subsea Tech Serv Inc | Methods for boosting hydrocarbon production |
| US6375437B1 (en) | 2000-02-04 | 2002-04-23 | Stanley Fastening Systems, Lp | Power operated air compressor assembly |
| US6394764B1 (en) | 2000-03-30 | 2002-05-28 | Dresser-Rand Company | Gas compression system and method utilizing gas seal control |
| US6843836B2 (en) | 2000-04-11 | 2005-01-18 | Cash Engineering Research Pty Ltd. | Integrated compressor drier apparatus |
| IT1319409B1 (en) | 2000-07-03 | 2003-10-10 | Nuovo Pignone Spa | EXHAUST SYSTEM FOR BEARINGS OF GAS TURBINES |
| US6761270B2 (en) | 2000-08-17 | 2004-07-13 | E. Bayne Carew | Wave coil filter assembly |
| SE0003915D0 (en) | 2000-10-27 | 2000-10-27 | Alfa Laval Ab | Centrifugal separator with rotor and drive for this |
| SE517663C2 (en) | 2000-10-27 | 2002-07-02 | Alfa Laval Corp Ab | Centrifugal separator for purification of a gaseous fluid |
| EP1333933B1 (en) | 2000-11-07 | 2006-02-01 | Shell Internationale Researchmaatschappij B.V. | Vertical cyclone separator |
| US6485536B1 (en) | 2000-11-08 | 2002-11-26 | Proteam, Inc. | Vortex particle separator |
| US6540917B1 (en) | 2000-11-10 | 2003-04-01 | Purolator Facet Inc. | Cyclonic inertial fluid cleaning apparatus |
| AU2002225701A1 (en) | 2000-11-14 | 2002-05-27 | Airex Corporation | Integrated magnetic bearing |
| JP3711028B2 (en) | 2001-02-20 | 2005-10-26 | 川崎重工業株式会社 | Gas turbine engine with foreign matter removal structure |
| US6402465B1 (en) | 2001-03-15 | 2002-06-11 | Dresser-Rand Company | Ring valve for turbine flow control |
| US6537035B2 (en) | 2001-04-10 | 2003-03-25 | Scott Shumway | Pressure exchange apparatus |
| US6547037B2 (en) | 2001-05-14 | 2003-04-15 | Dresser-Rand Company | Hydrate reducing and lubrication system and method for a fluid flow system |
| NL1018212C2 (en) | 2001-06-05 | 2002-12-10 | Siemens Demag Delaval Turbomac | Compressor unit comprising a centrifugal compressor and an electric motor. |
| US6669843B2 (en) | 2001-06-12 | 2003-12-30 | Hydrotreat, Inc. | Apparatus for mixing fluids |
| US7001448B1 (en) | 2001-06-13 | 2006-02-21 | National Tank Company | System employing a vortex finder tube for separating a liquid component from a gas stream |
| US6592654B2 (en) | 2001-06-25 | 2003-07-15 | Cryogenic Group Inc. | Liquid extraction and separation method for treating fluids utilizing flow swirl |
| US6599086B2 (en) | 2001-07-03 | 2003-07-29 | Marc S. C. Soja | Adjustable pump wear plate positioning assembly |
| JP2003047804A (en) | 2001-07-06 | 2003-02-18 | Honda Motor Co Ltd | Gas-liquid separation device |
| US6530979B2 (en) | 2001-08-03 | 2003-03-11 | Joseph Carl Firey | Flue gas cleaner |
| US6629816B2 (en) | 2001-08-16 | 2003-10-07 | Honeywell International Inc. | Non-contacting clearance seal for high misalignment applications |
| US6644400B2 (en) | 2001-10-11 | 2003-11-11 | Abi Technology, Inc. | Backwash oil and gas production |
| GB0124613D0 (en) | 2001-10-12 | 2001-12-05 | Alpha Thames Ltd | System and method for separating fluids |
| US6629825B2 (en) | 2001-11-05 | 2003-10-07 | Ingersoll-Rand Company | Integrated air compressor |
| AUPR912001A0 (en) | 2001-11-27 | 2001-12-20 | Rmg Services Pty. Ltd. | Advanced liquid vortex separation system |
| NL1019561C2 (en) | 2001-12-13 | 2003-06-17 | Frederic Pierre Joseph Koene | Cyclone separator as well as a liquid collection cabinet provided with such cyclone separators and a pressure vessel provided with such liquid collection boxes. |
| US6616719B1 (en) | 2002-03-22 | 2003-09-09 | Yung Yung Sun | Air-liquid separating method and apparatus for compressed air |
| DE10214863A1 (en) | 2002-04-04 | 2003-10-16 | Kloeckner Humboldt Wedag | cyclone |
| US7160518B2 (en) | 2002-04-11 | 2007-01-09 | Shell Oil Company | Cyclone separator |
| US6659143B1 (en) | 2002-05-31 | 2003-12-09 | Dresser, Inc. | Vapor recovery apparatus and method for gasoline dispensing systems |
| US6617731B1 (en) | 2002-06-05 | 2003-09-09 | Buffalo Pumps, Inc. | Rotary pump with bearing wear indicator |
| US6817846B2 (en) | 2002-06-13 | 2004-11-16 | Dresser-Rand Company | Gas compressor and method with improved valve assemblies |
| US6631617B1 (en) | 2002-06-27 | 2003-10-14 | Tecumseh Products Company | Two stage hermetic carbon dioxide compressor |
| US6698446B2 (en) | 2002-07-12 | 2004-03-02 | R. Conrader Company | Check valve |
| US7270145B2 (en) | 2002-08-30 | 2007-09-18 | Haldex Brake Corporation | unloading/venting valve having integrated therewith a high-pressure protection valve |
| NL1021656C2 (en) | 2002-10-15 | 2004-04-16 | Siemens Demag Delaval Turbomac | Compressor unit with common housing for electric motor and compressor, method for manufacturing a partition for a compressor unit and use of a compressor unit. |
| DE10251677A1 (en) | 2002-11-07 | 2004-05-19 | Mann + Hummel Gmbh | cyclone |
| DE10251940A1 (en) | 2002-11-08 | 2004-05-19 | Mann + Hummel Gmbh | Centrifugal oil separator for gas stream is used with blowby gases from crankcase of internal combustion engine has rotor shaped as centrifugal compressor with additional tangential outlet for oil |
| US7591882B2 (en) | 2002-12-02 | 2009-09-22 | Rerum Cognito Forschungszentrum Gmbh | Method for separating gas mixtures and a gas centrifuge for carrying out the method |
| ATE359488T1 (en) | 2003-01-07 | 2007-05-15 | Behr France Hambach Sarl | CAPACITOR WITH COLLECTION TANK AND PROTECTIVE CAP |
| DE10300729A1 (en) | 2003-01-11 | 2004-07-22 | Mann + Hummel Gmbh | Centrifugal oil separator |
| CA2457203C (en) | 2003-02-07 | 2008-04-08 | John R. Mckenzie | Apparatus and method for the removal of moisture and mists from gas flows |
| US6907933B2 (en) | 2003-02-13 | 2005-06-21 | Conocophillips Company | Sub-sea blow case compressor |
| SI1604115T1 (en) | 2003-03-10 | 2016-10-28 | Thermodyn | Integrated centrifugal compressor unit |
| US7063465B1 (en) | 2003-03-21 | 2006-06-20 | Kingsbury, Inc. | Thrust bearing |
| EP1613864B1 (en) | 2003-04-11 | 2015-10-14 | Thermodyn | Centrifugal motor-compressor unit |
| US7014756B2 (en) | 2003-04-18 | 2006-03-21 | Genoil Inc. | Method and apparatus for separating immiscible phases with different densities |
| US7025890B2 (en) | 2003-04-24 | 2006-04-11 | Griswold Controls | Dual stage centrifugal liquid-solids separator |
| US6718955B1 (en) | 2003-04-25 | 2004-04-13 | Thomas Geoffrey Knight | Electric supercharger |
| US6878187B1 (en) | 2003-04-29 | 2005-04-12 | Energent Corporation | Seeded gas-liquid separator and process |
| DE60333599D1 (en) | 2003-05-16 | 2010-09-09 | Haimo Technologies Inc | ADJUSTABLE GAS LIQUID CENTRIFUGAL SEPARATOR AND SEPARATION METHOD |
| US7080690B2 (en) | 2003-06-06 | 2006-07-25 | Reitz Donald D | Method and apparatus using traction seal fluid displacement device for pumping wells |
| KR100565341B1 (en) | 2003-06-20 | 2006-03-30 | 엘지전자 주식회사 | Dust separation device of cyclone cleaner |
| NO323324B1 (en) | 2003-07-02 | 2007-03-19 | Kvaerner Oilfield Prod As | Procedure for regulating that pressure in an underwater compressor module |
| DE502004002264D1 (en) | 2003-07-05 | 2007-01-25 | Man Turbo Ag Schweiz | Compressor device and method of operating the same |
| US7594942B2 (en) | 2003-09-09 | 2009-09-29 | Shell Oil Company | Gas/liquid separator |
| NO321304B1 (en) | 2003-09-12 | 2006-04-24 | Kvaerner Oilfield Prod As | Underwater compressor station |
| SE525981C2 (en) | 2003-10-07 | 2005-06-07 | 3Nine Ab | Device at a centrifugal separator |
| TWI285562B (en) | 2003-10-10 | 2007-08-21 | Tama Tlo Corp | Cyclone type centrifugal separating apparatus |
| US7112036B2 (en) | 2003-10-28 | 2006-09-26 | Capstone Turbine Corporation | Rotor and bearing system for a turbomachine |
| DE10358030A1 (en) | 2003-12-11 | 2005-07-07 | Hilti Ag | cyclone |
| AT413339B (en) | 2003-12-30 | 2006-02-15 | Pmt Gesteinsvermahlungstechnik | LEADING DEVICE FOR FLOWERS, ESPECIALLY CYCLONE SEPARATORS |
| US7131292B2 (en) | 2004-02-18 | 2006-11-07 | Denso Corporation | Gas-liquid separator |
| US7377110B2 (en) | 2004-03-31 | 2008-05-27 | United Technologies Corporation | Deoiler for a lubrication system |
| AT413080B (en) | 2004-04-29 | 2005-11-15 | Arbeiter Peter | DRYING DEVICE |
| GB0414344D0 (en) | 2004-06-26 | 2004-07-28 | Rolls Royce Plc | Centrifugal gas/liquid separators |
| US7258713B2 (en) | 2004-08-27 | 2007-08-21 | Dreison International, Inc. | Inlet vane for centrifugal particle separator |
| US7204241B2 (en) | 2004-08-30 | 2007-04-17 | Honeywell International, Inc. | Compressor stage separation system |
| GB2417702B (en) | 2004-09-01 | 2007-10-24 | Bissell Homecare Inc | Cyclone separator with fine particle separation member |
| US7241392B2 (en) | 2004-09-09 | 2007-07-10 | Dresser-Rand Company | Rotary separator and method |
| US7497666B2 (en) | 2004-09-21 | 2009-03-03 | George Washington University | Pressure exchange ejector |
| JP2006097585A (en) | 2004-09-29 | 2006-04-13 | Mitsubishi Heavy Ind Ltd | Mounting structure for air separator and gas turbine provided with the same |
| US20060065609A1 (en) | 2004-09-30 | 2006-03-30 | Arthur David J | Fluid control device |
| US7288202B2 (en) | 2004-11-08 | 2007-10-30 | Dresser-Rand Company | Rotary separator and method |
| US20070051245A1 (en) | 2005-02-03 | 2007-03-08 | Jangshik Yun | Wet type air purification apparatus utilizing a centrifugal impeller |
| EP1851438B1 (en) | 2005-02-26 | 2015-04-22 | Ingersoll-Rand Company | System and method for controlling a variable speed compressor during stopping |
| US8075668B2 (en) | 2005-03-29 | 2011-12-13 | Dresser-Rand Company | Drainage system for compressor separators |
| KR100594587B1 (en) | 2005-03-29 | 2006-06-30 | 삼성광주전자 주식회사 | Multi Cyclone Dust Collector |
| KR100607442B1 (en) | 2005-03-29 | 2006-08-02 | 삼성광주전자 주식회사 | Multi cyclone dust collector and vacuum cleaner using the same |
| KR100611067B1 (en) | 2005-04-18 | 2006-08-10 | 삼성광주전자 주식회사 | Cyclone dust collector for vacuum cleaner and vacuum cleaner having same |
| WO2006119737A1 (en) | 2005-05-10 | 2006-11-16 | Mahle International Gmbh | Centrifugal oil mist separation device integrated in an axial hollow shaft of an internal combustion engine |
| GB2463820B (en) | 2005-05-17 | 2010-06-09 | Thomas Industries Inc | Pump Improvements |
| SE528701C2 (en) | 2005-06-08 | 2007-01-30 | Alfa Laval Corp Ab | Centrifugal separator for purification of a gas |
| SE528750C2 (en) | 2005-06-27 | 2007-02-06 | 3Nine Ab | Method and apparatus for separating particles from a gas stream |
| GB0515266D0 (en) | 2005-07-26 | 2005-08-31 | Domnick Hunter Ltd | Separator assembly |
| US7442006B2 (en) | 2005-08-15 | 2008-10-28 | Honeywell International Inc. | Integral diffuser and deswirler with continuous flow path deflected at assembly |
| CN101268282B (en) | 2005-09-19 | 2013-10-16 | 英格索尔-兰德公司 | Fluid compression system |
| US7677308B2 (en) | 2005-09-20 | 2010-03-16 | Tempress Technologies Inc | Gas separator |
| NO325900B1 (en) | 2005-10-07 | 2008-08-11 | Aker Subsea As | Apparatus and method for controlling the supply of barrier gas to a compressor module |
| WO2007064605A2 (en) | 2005-11-30 | 2007-06-07 | Dresser-Rand Company | End closure device for a turbomachine casing |
| JP2007162561A (en) | 2005-12-13 | 2007-06-28 | Toyota Industries Corp | Refrigerant compressor |
| US7621973B2 (en) | 2005-12-15 | 2009-11-24 | General Electric Company | Methods and systems for partial moderator bypass |
| US20070151922A1 (en) | 2006-01-05 | 2007-07-05 | Mian Farouk A | Spiral Speed Separator (SSS) |
| SE529611C2 (en) | 2006-02-13 | 2007-10-02 | Alfa Laval Corp Ab | centrifugal |
| SE529609C2 (en) | 2006-02-13 | 2007-10-02 | Alfa Laval Corp Ab | centrifugal |
| SE529610C2 (en) | 2006-02-13 | 2007-10-02 | Alfa Laval Corp Ab | centrifugal |
| US7744663B2 (en) | 2006-02-16 | 2010-06-29 | General Electric Company | Methods and systems for advanced gasifier solids removal |
| ITMI20060294A1 (en) | 2006-02-17 | 2007-08-18 | Nuovo Pignone Spa | MOTOCOMPRESSORE |
| EP1993692B1 (en) | 2006-03-03 | 2016-08-24 | Dresser-Rand Company | Multiphase fluid processing device |
| KR20070093638A (en) | 2006-03-14 | 2007-09-19 | 엘지전자 주식회사 | Oil separator of scroll compressor |
| FR2899288B1 (en) | 2006-03-30 | 2008-06-13 | Total Sa | METHOD AND DEVICE FOR COMPRESSION OF A MULTIPHASIC FLUID |
| CA2647511C (en) | 2006-03-31 | 2013-01-29 | Dresser-Rand Company | Control valve assembly for a compressor unloader |
| US20100043364A1 (en) | 2006-04-04 | 2010-02-25 | Winddrop | Liquid-gas separator, namely for vacuum cleaner |
| DE202006006085U1 (en) | 2006-04-12 | 2007-08-16 | Mann+Hummel Gmbh | Multi-stage device for separating drops of liquid from gases |
| US7628836B2 (en) | 2006-05-08 | 2009-12-08 | Hamilton Sundstrand Corporation | Rotary drum separator system |
| WO2008014688A1 (en) | 2006-07-26 | 2008-02-07 | Xiaoying Yun | A rotary piston compressor |
| US7594941B2 (en) | 2006-08-23 | 2009-09-29 | University Of New Brunswick | Rotary gas cyclone separator |
| CA2664121C (en) | 2006-09-19 | 2014-05-27 | William C. Maier | Rotary separator drum seal |
| WO2008036394A2 (en) | 2006-09-21 | 2008-03-27 | Dresser-Rand Company | Separator drum and compressor impeller assembly |
| EP2066948A4 (en) | 2006-09-25 | 2012-01-11 | Dresser Rand Co | Access cover for pressurized connector spool |
| CA2663883C (en) | 2006-09-25 | 2015-02-03 | Kevin M. Majot | Coupling guard system |
| US8231336B2 (en) | 2006-09-25 | 2012-07-31 | Dresser-Rand Company | Fluid deflector for fluid separator devices |
| BRPI0717090A8 (en) | 2006-09-25 | 2017-09-12 | Dresser Rand Co | COMPRESSOR ASSEMBLY SYSTEM |
| CA2662780C (en) | 2006-09-25 | 2015-02-03 | William C. Maier | Axially moveable spool connector |
| BRPI0717253B1 (en) | 2006-09-26 | 2018-05-08 | Dresser Rand Co | fluid separator |
| US7520210B2 (en) | 2006-09-27 | 2009-04-21 | Visteon Global Technologies, Inc. | Oil separator for a fluid displacement apparatus |
| JP4875484B2 (en) | 2006-12-28 | 2012-02-15 | 三菱重工業株式会社 | Multistage compressor |
| US7948105B2 (en) | 2007-02-01 | 2011-05-24 | R&D Dynamics Corporation | Turboalternator with hydrodynamic bearings |
| US7637699B2 (en) | 2007-07-05 | 2009-12-29 | Babcock & Wilcox Power Generation Group, Inc. | Steam/water conical cyclone separator |
| US7708808B1 (en) | 2007-06-01 | 2010-05-04 | Fisher-Klosterman, Inc. | Cyclone separator with rotating collection chamber |
| DE102007028935B4 (en) | 2007-06-22 | 2018-12-27 | Saurer Spinning Solutions Gmbh & Co. Kg | Method and device for starting an electric machine with a magnetically mounted rotor |
| DE102007032933B4 (en) | 2007-07-14 | 2015-02-19 | Atlas Copco Energas Gmbh | turbomachinery |
| JP2009047039A (en) | 2007-08-17 | 2009-03-05 | Mitsubishi Heavy Ind Ltd | Multistage compressor |
| US8066077B2 (en) | 2007-12-17 | 2011-11-29 | Baker Hughes Incorporated | Electrical submersible pump and gas compressor |
| US7757866B2 (en) | 2007-12-20 | 2010-07-20 | Mccutchen Co. | Rotary annular crossflow filter, degasser, and sludge thickener |
| US7811344B1 (en) | 2007-12-28 | 2010-10-12 | Bobby Ray Duke | Double-vortex fluid separator |
| US7708537B2 (en) | 2008-01-07 | 2010-05-04 | Visteon Global Technologies, Inc. | Fluid separator for a compressor |
| GB2470151B (en) | 2008-03-05 | 2012-10-03 | Dresser Rand Co | Compressor assembly including separator and ejector pump |
| US7846228B1 (en) | 2008-03-10 | 2010-12-07 | Research International, Inc. | Liquid particulate extraction device |
| US8079805B2 (en) | 2008-06-25 | 2011-12-20 | Dresser-Rand Company | Rotary separator and shaft coupler for compressors |
| US8062400B2 (en) | 2008-06-25 | 2011-11-22 | Dresser-Rand Company | Dual body drum for rotary separators |
| US8899912B2 (en) | 2009-01-15 | 2014-12-02 | Dresser-Rand Company | Shaft seal with convergent nozzle |
| US8061970B2 (en) | 2009-01-16 | 2011-11-22 | Dresser-Rand Company | Compact shaft support device for turbomachines |
| US8087901B2 (en) | 2009-03-20 | 2012-01-03 | Dresser-Rand Company | Fluid channeling device for back-to-back compressors |
| US8210804B2 (en) | 2009-03-20 | 2012-07-03 | Dresser-Rand Company | Slidable cover for casing access port |
| US8061972B2 (en) | 2009-03-24 | 2011-11-22 | Dresser-Rand Company | High pressure casing access cover |
| BR112012005866B1 (en) | 2009-09-15 | 2021-01-19 | Dresser-Rand Company | apparatus for separating a fluid and method for separating a component of higher specific weight from a component of lower specific weight of a fluid |
-
2008
- 2008-06-25 US US12/215,184 patent/US7922218B2/en not_active Expired - Fee Related
-
2009
- 2009-06-24 BR BRPI0901998-7A patent/BRPI0901998A2/en not_active Application Discontinuation
-
2011
- 2011-01-20 US US13/010,465 patent/US8430433B2/en not_active Expired - Fee Related
Patent Citations (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1622768A (en) * | 1924-06-04 | 1927-03-29 | Cook Henry Denman | Pipe joint and connection |
| US2328031A (en) * | 1941-06-27 | 1943-08-31 | Dresser Mfg Company | Pipe clamp and method and apparatus for applying same |
| US2836117A (en) * | 1954-07-06 | 1958-05-27 | Harry G Lankford | Clamp means |
| US2868565A (en) * | 1956-05-01 | 1959-01-13 | George E Suderow | Releasable pivoted clamp for joining internally flanged structural members |
| US3044657A (en) * | 1957-06-14 | 1962-07-17 | Richard H Horton | Flange and wall structure |
| US3220245A (en) * | 1963-03-25 | 1965-11-30 | Baker Oil Tools Inc | Remotely operated underwater connection apparatus |
| US3352577A (en) * | 1967-06-27 | 1967-11-14 | Koppers Co Inc | Coupling arrangement for filament reinforced thermosetting resin tubular members |
| US3628812A (en) * | 1969-12-01 | 1971-12-21 | Exxon Production Research Co | Removable pipe connector |
| US4146261A (en) * | 1977-02-12 | 1979-03-27 | Motoren- Und Turbinen-Union Friedrichshafen Gmbh | Clamping arrangement |
| US4205927A (en) * | 1977-12-16 | 1980-06-03 | Rolls-Royce Limited | Flanged joint structure for composite materials |
| US4573527A (en) * | 1983-07-29 | 1986-03-04 | Mcdonough M J | Heat exchanger closure connection |
| US4984830A (en) * | 1988-11-02 | 1991-01-15 | Cooper Industries, Inc. | Collet type connector |
| US5024585A (en) * | 1990-04-09 | 1991-06-18 | Sta-Rite Industries, Inc. | Housing coupling mechanism |
| US5443581A (en) * | 1992-12-03 | 1995-08-22 | Wood George & Co., Inc. | Clamp assembly for clamp hub connectors and a method of installing the same |
| US5967746A (en) * | 1997-07-30 | 1999-10-19 | Mitsubishi Heavy Industries, Ltd. | Gas turbine interstage portion seal device |
| US5951066A (en) * | 1998-02-23 | 1999-09-14 | Erc Industries, Inc. | Connecting system for wellhead components |
| US6123363A (en) * | 1998-11-02 | 2000-09-26 | Uop Llc | Self-centering low profile connection with trapped gasket |
| US6715802B2 (en) * | 1999-10-18 | 2004-04-06 | William J. Baker | Apparatus for connecting tubular bodies |
| US6467988B1 (en) * | 2000-05-20 | 2002-10-22 | General Electric Company | Reducing cracking adjacent shell flange connecting bolts |
| US6688802B2 (en) * | 2001-09-10 | 2004-02-10 | Siemens Westinghouse Power Corporation | Shrunk on industrial coupling without keys for industrial system and associated methods |
| US6764284B2 (en) * | 2002-01-10 | 2004-07-20 | Parker-Hannifin Corporation | Pump mount using sanitary flange clamp |
| US6658986B2 (en) * | 2002-04-11 | 2003-12-09 | Visteon Global Technologies, Inc. | Compressor housing with clamp |
| US7527306B2 (en) * | 2002-05-30 | 2009-05-05 | Arkal Filtration Systems C.S. Ltd. | Pipe coupling |
| US6824171B2 (en) * | 2002-08-23 | 2004-11-30 | Dril-Quip, Inc. | Riser connector |
| US7481464B2 (en) * | 2006-06-08 | 2009-01-27 | Karl Hamacher Gmbh | Coupling, particularly pipe coupling for high-pressure pipes or hoses |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100270308A1 (en) * | 2009-04-22 | 2010-10-28 | Hitachi Plant Technologies, Ltd. | End wall closure apparatus |
| US8631961B2 (en) * | 2009-04-22 | 2014-01-21 | Hitachi, Ltd. | End wall closure apparatus |
| US11085373B2 (en) * | 2019-01-31 | 2021-08-10 | Rolls-Royce North American Technologies Inc. | Gas turbine engine with mount for interchangeable inlets |
Also Published As
| Publication number | Publication date |
|---|---|
| US7922218B2 (en) | 2011-04-12 |
| US8430433B2 (en) | 2013-04-30 |
| US20110158802A1 (en) | 2011-06-30 |
| BRPI0901998A2 (en) | 2010-04-13 |
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